CN108177790A - A kind of unmanned plane relay station and its method - Google Patents
A kind of unmanned plane relay station and its method Download PDFInfo
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- CN108177790A CN108177790A CN201810121999.3A CN201810121999A CN108177790A CN 108177790 A CN108177790 A CN 108177790A CN 201810121999 A CN201810121999 A CN 201810121999A CN 108177790 A CN108177790 A CN 108177790A
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- 238000000034 method Methods 0.000 title claims abstract description 18
- 238000009434 installation Methods 0.000 claims abstract description 19
- 230000000284 resting effect Effects 0.000 claims abstract description 15
- 230000000694 effects Effects 0.000 claims abstract description 12
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 19
- 230000005611 electricity Effects 0.000 claims description 8
- 229910052742 iron Inorganic materials 0.000 claims description 8
- 238000011900 installation process Methods 0.000 claims description 3
- 230000005662 electromechanics Effects 0.000 claims 2
- 235000008331 Pinus X rigitaeda Nutrition 0.000 claims 1
- 235000011613 Pinus brutia Nutrition 0.000 claims 1
- 241000018646 Pinus brutia Species 0.000 claims 1
- 230000001846 repelling effect Effects 0.000 claims 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 3
- 238000003780 insertion Methods 0.000 description 2
- 230000037431 insertion Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000001133 acceleration Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000295 fuel oil Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
-
- 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
- B60L53/80—Exchanging energy storage elements, e.g. removable batteries
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/12—Ground or aircraft-carrier-deck installations for anchoring aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U80/00—Transport or storage specially adapted for UAVs
- B64U80/80—Transport or storage specially adapted for UAVs by vehicles
- B64U80/86—Land vehicles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Remote Sensing (AREA)
- Power Engineering (AREA)
- Vehicle Cleaning, Maintenance, Repair, Refitting, And Outriggers (AREA)
- Battery Mounting, Suspending (AREA)
Abstract
The invention discloses a kind of unmanned plane relay stations to include relay station ontology, unmanned plane unit, unmanned plane battery roll unit and unmanned machine battery installation unit；Unmanned plane unit, which rests, is installed on relay station car body top；Unmanned plane battery roll unit and unmanned machine battery installation unit are additionally provided on relay station car body, unmanned plane battery roll unit and unmanned machine battery installation unit are located at side before and after the unmanned plane unit of resting state respectively, relay station bodies top has been horizontally disposed with unmanned plane and has rested frame, and driving device, which can drive, rests frame horizontal rotation；The structure of the present invention is simple, it rests in rotatable unmanned plane and triangle chuck is set on frame, structure makes under unmanned plane resting state, it realizes and is accurately positioned under the premise of retaining certain serious forgiveness, and resting state is in clamped condition, firm position, while unmanned plane power battery is installed in the form of electromagnetic launch, have the characteristics that process is rapid, realize the quick main automatic effect for replacing battery.
Description
Technical field
The invention belongs to unmanned plane field more particularly to a kind of unmanned plane relay station and its methods.
Background technology
Unmanned plane using battery as power has the excellent performances such as light and handy, flexible, acceleration height, but using battery as power
Unmanned plane often cruising ability is weak compared with fuel oil unmanned plane very much；However it is existing using battery as the unmanned plane of power, generally
Using stopping flight after battery is exhausted, it is therefore desirable to a kind of relay station that can replace battery.
Invention content
Goal of the invention：In order to overcome the deficiencies in the prior art, the present invention provides the one of a kind of automatic replacement battery
Kind unmanned plane relay station and its method.
Technical solution：To achieve the above object, a kind of unmanned plane relay station of the invention includes relay station ontology, unmanned plane
Unit, unmanned plane battery roll unit and unmanned machine battery installation unit；
The unmanned plane unit, which rests, is installed on the relay station car body top；Nothing is additionally provided on the relay station car body
Man-machine battery roll unit and unmanned machine battery installation unit, the unmanned plane battery roll unit and the installation of unmanned machine battery are single
Member is located at side before and after the unmanned plane unit of resting state respectively.
Further, the relay station bodies top has been horizontally disposed with unmanned plane and has rested frame, and driving device can drive and rest
Frame rotates horizontally；The unmanned plane unit, which rests, to be installed on the unmanned plane and rests on frame；
Battery mounting base is provided on the downside of the unmanned plane unit, unmanned plane power battery is slid horizontally into from side to be installed on
In the battery mounting base, and the end of slipping into of unmanned plane power battery is provided with battery out splice going splice, the battery out splice going splice
It is corresponding to be inserted into the power interface on the inside of the battery mounting base；Battery mounting base can be driven by rotating the unmanned plane and resting frame
Battery skids off end and is rotated successively to corresponding with unmanned plane battery roll unit and unmanned machine battery installation unit respectively.
Further, four of the unmanned plane unit rest support feet and are arranged to cylinder；The unmanned plane rests frame
In decussation structure, the unmanned plane rest frame quadrangle on the upside of be separately installed with four scroll chucks；The unmanned plane
Support feet of resting described in four of unit distinguishes concentric correspondence in four scroll chucks；Each scroll chuck can press from both sides
The corresponding support feet of resting of tight or release.
Further, the both sides of the unmanned plane power battery are provided with draw runner along its length；The battery installation
Draw runner guide groove is provided on seat, two draw runners are slideably positioned in respectively in the corresponding draw runner guide groove；The unmanned plane
Magnetic component is provided on the upside of power battery；It is provided in the battery mounting base and unmanned plane power battery corresponding
One permanent magnet, the first permanent magnet magnetic connect the magnetic component of the upside of the unmanned plane power battery.
Further, the unmanned plane rests and is also installed with ejection guiding device on frame；The ejection guiding device is edge
The box structure of length direction perforation, the ejection guiding device inside is battery guiding channel；
The battery guiding channel skids off end with the battery of the battery mounting base and docks setting；From the battery mounting base
In skid off unmanned plane power battery correspondence slip into the battery guiding channel；The two madial wall upper edge of battery guiding channel
Battery skids off direction and has been extended draw runner guiding groove, and two draw runners on unmanned plane power battery guide respectively with two draw runners
Slot is correspondingly arranged.
Further, unmanned plane power battery is installed in the battery mounting base under state, the unmanned plane power electric
Pond skids off end side close to the battery of the battery mounting base and is provided with the second permanent magnet.
Further, the unmanned plane battery roll unit includes dismounting platform；It is passed through before and after being set on the dismounting platform
Logical electromagnetism placing groove, the one end of the battery placing groove far from the unmanned plane unit are provided with cylinder block, the cylinder block
One end of the unmanned plane unit is provided with telescopic cylinder, the telescopic cylinder is along perforation side before and after the battery placing groove
To extension, the telescopic cylinder end is provided with the first electromagnet, and the telescopic cylinder can drive the first electromagnet to extend out to nothing
At the battery mounting base of man-machine unit, telescopic cylinder can also drive the first electromagnet to be retracted in battery placing groove；Described first
Under electromagnet energized state, the first electromagnet and the second permanent magnet in the battery mounting base on unmanned plane power battery are mutual
Magnetic.
Further, the unmanned machine battery installation unit includes battery ejection case, the second electromagnet and the second electromagnet
Fixed seat；
The battery ejection case is body structure；The intracavity bottom of the battery ejection case is provided with longitudinal spring, described
Several unmanned plane power batteries for stacking setting of upper end top pressure of longitudinal spring；
Second electromagnet is fixedly installed in the battery by the second electromagnet fixed seat and launches on the outside of case, and described
Second electromagnet is located at side of the battery ejection case far from the unmanned plane unit；The battery launches case close to the nothing
The side upper end of man-machine unit offers ejection opening, and the ejection opening is correspondingly arranged with second electromagnet；Second electricity
Under magnet energized state, the second permanent magnet that the second electromagnet is launched with battery on Xiang Zhong top layers unmanned plane power battery is mutual
Repel, the battery ejection Xiang Zhong top layers unmanned plane power battery can be through in ejection opening pop-up to battery guiding channel.
Further, a kind of method of unmanned plane relay station：
During unmanned plane during flying state, stop the serious forgiveness of pick-up point to ensure that its unmanned plane unit makes a return voyage, each scroll chuck
Chuck motor driving radially movable to the maximum open configuration of movable jaw, in unmanned plane unit normal flight operations, institute
When carrying the electricity of unmanned plane power battery will exhaust, at this moment controller control unmanned plane unit makes a return voyage, the unmanned plane of flight
Unit is gradually flown to right over relay station ontology, controls the slow vertical landing of unmanned plane unit of flight at this time, until unmanned plane
Four of unit are rested support feet and are stretched into the scroll chuck of corresponding four open configurations, and unmanned plane unit has been completed at this time
Landing, starts the chuck motor of one of scroll chuck, makes three movable jaws of its single scroll chuck radially at this time
Pinching action inwardly is done, treats to clamp completely to rest to suspend before support feet and continues to clamp, drives second scroll chuck at this time
Chuck motor makes three movable jaws of its second scroll chuck do pinching action radially inward, treats to clamp completely and rest
Suspend before support feet and continue to clamp；Unmanned plane unit is basically completed positioning at this time, continues in this way at this time successively
The chuck motor of three, the 4th scroll chucks simultaneously does pinching action；Then the chuck motor of four scroll chucks is driven simultaneously
It is made to clamp four completely respectively and rests support feet, unmanned plane unit has been fully positioned at unmanned plane and has rested on frame at this time；
The unmanned plane of driving device driving at this time rests frame horizontal rotation, and the battery of battery mounting base is made to skid off end rotation to court
To dismounting platform, the battery of battery mounting base that telescopic cylinder drives the first electromagnet to extend out to unmanned plane unit is driven to slide at this time
At outlet, then the first electromagnet is given to be powered, at this time the first electromagnet in battery mounting base on unmanned plane power battery the
Two permanent magnets attract each other；Then driving telescopic cylinder drives the first electromagnet gradually to do retract action, at this time battery mounting base
In unmanned plane power battery due to by magnetic pulling force, the power supply that battery out splice going splice starts to be detached from the inside of battery mounting base connects
Mouthful, and unmanned plane power battery is in the first electromagnet together retraction movement to battery placing groove, and unmanned plane unit has been at this time
Through completing battery roll process；
Further, driving device driving unmanned plane rest frame horizontal rotation, make battery mounting base battery skid off end rotation
Go to the ejection opening towards battery ejection case；The second electromagnet is powered by moment at this time, and then the second battery iron and battery bullet
The second permanent magnet moment on She Xiangzhong top layers unmanned plane power battery generates strong repulsive forces, and then in battery ejection case most
Upper strata unmanned plane power battery is launched away rapidly under repulsive force effect from ejection opening, and ejection process once occurs immediately
By the second electromagnet power off, battery ejection case in former second layer unmanned plane power battery move up under the action of the spring with
Second electromagnet is equal, preparation launched again, by the unmanned plane power battery that ejection is gone out battery guiding channel guiding
Battery mounting base is slided under effect, the unmanned plane power battery skidded off from battery guiding channel is skidded off from the battery of battery mounting base
End is slipped into battery mounting base, and the battery out splice going splice of unmanned plane power battery corresponds to insertion battery peace under effect of inertia
It fills in seat upper power source interface, the automatic magnetic of the first permanent magnet connects the magnetic part of the upside of the unmanned plane power battery at this time
Part, the magnetic attraction of the magnetic component further prevent nobody much smaller than the repulsive force between the second battery iron and the second permanent magnet
It is skidded off automatically in mechanomotive force battery flight course, realizes the installation process of battery；Then driving four scroll chucks simultaneously
Chuck motor makes it be totally released four to rest support feet, finally unmanned plane unit is driven to take off vertically.
Advantageous effect：The structure of the present invention is simple, rests in rotatable unmanned plane and sets triangle chuck on frame, structure makes
It under unmanned plane resting state, realizes and is accurately positioned under the premise of retaining certain serious forgiveness, and resting state is in clamped condition,
Firm position, while unmanned plane power battery is installed in the form of electromagnetic launch, have the characteristics that process is rapid, realize quick
The main automatic effect for replacing battery.
Description of the drawings
Attached drawing 1 is overall structure diagram of the present invention；
Attached drawing 2 is vertical view of the present invention；
Attached drawing 3 launches case internal structure schematic diagram for battery；
Attached drawing 4 rests frame structure diagram for unmanned plane；
Attached drawing 5 is unmanned plane unit disassembling the first view of cell process；
Attached drawing 6 is unmanned plane unit disassembling the second view of cell process；
Attached drawing 7 is unmanned plane element cell seat partial bottom view.
Specific embodiment
The present invention is further described below in conjunction with the accompanying drawings.
1st, the introduction about the construction of this programme：
A kind of unmanned plane relay station as described in attached drawing 1 to 7, including relay station ontology 18, unmanned plane unit 11, unmanned plane
Battery roll unit and unmanned machine battery installation unit；The unmanned plane unit 11, which rests, to be installed on the relay station car body 18 and pushes up
Portion；Be additionally provided with unmanned plane battery roll unit and unmanned machine battery installation unit on the relay station car body 18, it is described nobody
Machine battery removable unit and unmanned machine battery installation unit are located at side before and after the unmanned plane unit 11 of resting state respectively；Institute
It states 18 top horizontal of relay station ontology and is provided with unmanned plane and rest frame 28, driving device, which can drive, rests frame 28 and rotate horizontally；Institute
It states unmanned plane unit 11 and rests and be installed on the unmanned plane and rest on frame 28；
The downside of unmanned plane unit 11 in the present embodiment is provided with battery mounting base 22, and unmanned plane power battery 3 is from side
It is slid horizontally into and is installed in the battery mounting base 22, and the end of slipping into of unmanned plane power battery 3 is provided with battery out splice going splice
1, the battery out splice going splice 1, which corresponds to, to be inserted into the power interface 12 of 22 inside of battery mounting base；Rotate the unmanned plane
The frame 28 that rests can drive the battery of battery mounting base 22 skid off end 22.1 rotate successively to respectively with unmanned plane battery roll unit
It is corresponding with unmanned machine battery installation unit.
Four of unmanned plane unit 11 in the present embodiment rest support feet 10 and are arranged to cylinder；The unmanned plane rests
Frame 28 be in decussation structure, the unmanned plane rest frame 28 quadrangle on the upside of be separately installed with four scroll chucks 14；Institute
It states and rests support feet 10 described in four of unmanned plane unit 11 and distinguish concentric correspondence in four scroll chucks 14；Each institute
It states scroll chuck 14 and may tighten or loosen the corresponding support feet 10 of resting.
The both sides of the unmanned plane power battery 3 are provided with draw runner 2 along its length；It is set on the battery mounting base 22
Draw runner guide groove 43 is equipped with, two draw runners 2 are slideably positioned in respectively in the corresponding draw runner guide groove 43；It is described that nobody is motor-driven
The upside of power battery 3 is provided with magnetic component；It is provided in the battery mounting base 22 corresponding with unmanned plane power battery 3
First permanent magnet 19,19 magnetic of the first permanent magnet connect the magnetic component of the upside of the unmanned plane power battery 3.
The unmanned plane, which rests, is also installed with ejection guiding device 25 on frame 28；The ejection guiding device 25 is along length
The box structure of direction perforation, 25 inside of ejection guiding device is battery guiding channel 32；
The battery guiding channel 32 skids off end 22.1 with the battery of the battery mounting base 22 and docks setting；From the electricity
The correspondence of unmanned plane power battery 3 skidded off in pond mounting base 22 is slipped into the battery guiding channel 32；The battery guiding is logical
32 liang of road madial wall upper edge battery skids off direction and has been extended draw runner guiding groove 33, two draw runners 2 on unmanned plane power battery 3
It is correspondingly arranged respectively with the two draw runner guiding grooves 33.
Unmanned plane power battery 3 in the present embodiment is installed in the battery mounting base 22 under state, the unmanned plane
Power battery 3 skids off 22.1 sides of end close to the battery of the battery mounting base 22 and is provided with the second permanent magnet 3.1.
The unmanned plane battery roll unit in the present embodiment includes dismounting platform 30.1；On the dismounting platform 30.1
The front and rear electromagnetism placing groove 30 penetrated through of setting, the one end of the battery placing groove 30 far from the unmanned plane unit 11 is provided with gas
Cylinder seat 16, the cylinder block 16 are provided with telescopic cylinder 15, the telescopic cylinder 15 close to one end of the unmanned plane unit 11
Along the front and rear perforation direction extension of the battery placing groove 30,15 end of telescopic cylinder is provided with the first electromagnet 29, described
Telescopic cylinder 15 can drive the first electromagnet 29 to extend out at the battery mounting base 22 of unmanned plane unit 11, and telescopic cylinder 15 may be used also
The first electromagnet 29 is driven to be retracted in battery placing groove 30；Under first electromagnet, 29 energized state, using opposite pole
Attracting principle, the first electromagnet 29 and 3.1 phase of the second permanent magnet in the battery mounting base 22 on unmanned plane power battery 3
Mutual magnetic.
The unmanned machine battery installation unit in the present embodiment includes battery ejection case 27, the second electromagnet 26 and second
Electromagnet fixed seat 45；The battery ejection case 27 is body structure；The intracavity bottom of the battery ejection case 27 is provided with vertical
To spring 46, several unmanned plane power batteries 3 for stacking setting of upper end top pressure of the longitudinal spring 46；
Second electromagnet 26 is fixedly installed in the battery by the second electromagnet fixed seat 45 and launches 27 outside of case,
And second electromagnet 26 is located at side of the battery ejection case 27 far from the unmanned plane unit 11；The battery ejection
Case 27 offers ejection opening 3.2, the ejection opening 3.2 and described second close to the side upper end of the unmanned plane unit 11
Electromagnet 26 is correspondingly arranged；Under second electromagnet, 26 energized state, the principle mutually repelled using like pole, the second electromagnet 26
The second permanent magnet 3.1 launched with battery in case 27 on top layer's unmanned plane power battery 3 is mutually exclusive, and the battery launches case
Top layer's unmanned plane power battery 3 can be through in 3.2 pop-up to battery guiding channel 32 of ejection opening in 27.
2nd, the method for this programme, process, principle and technological progress arrange as follows：
During unmanned plane during flying state, stop the serious forgiveness of pick-up point to ensure that its unmanned plane unit 11 makes a return voyage, each three-jaw card
The chuck motor 17 of disk 14 drives radially movable to the maximum open configuration of movable jaw, in 11 normal flight mistake of unmanned plane unit
Cheng Zhong, when the electricity of entrained unmanned plane power battery 3 will exhaust, at this moment controller control unmanned plane unit 11 makes a return voyage, and flies
Capable unmanned plane unit 11 is gradually flown to right over relay station ontology 18, and the unmanned plane unit 11 for controlling flight at this time is slowly vertical
Landing, until four of unmanned plane unit 11 rest support feet 10 and stretch into the scroll chuck 14 of corresponding four open configurations,
Unmanned plane unit has been completed to land at this time, starts the chuck motor 17 of one of scroll chuck 14 at this time, make its single three
Three movable jaws of dog chuck 14 do pinching action radially inward, treat to clamp completely to rest to suspend before support feet 10 and continue
It clamps, drives the chuck motor 17 of second scroll chuck 14 at this time, make three movable jaws of its second scroll chuck 14
Pinching action is done radially inward, is treated to clamp completely to rest to suspend before support feet 10 and is continued to clamp；Unmanned plane unit 11 at this time
Be basically completed positioning, continue in this way at this time successively by third, the 4th scroll chuck 14 chuck motor 17 and do
Pinching action；Then it drives the chuck motor 17 of four scroll chucks 14 that it is made to clamp four completely respectively simultaneously and rests support feet
10, at this time unmanned plane unit 11 be fully positioned at unmanned plane and rested on frame 28；
The unmanned plane of driving device driving at this time rests frame 28 and rotates horizontally, and the battery of battery mounting base 22 is made to skid off end 22.1
Rotation drives telescopic cylinder 15 that the first electromagnet 29 is driven to extend out to unmanned plane unit 11 at this time to towards dismounting platform 30.1
The battery of battery mounting base 22 is skidded off at end 22.1, is then powered to the first electromagnet 29, the first electromagnet 29 is in battery at this time
The second permanent magnet 3.1 in mounting base 22 on unmanned plane power battery 3 attracts each other；Then driving telescopic cylinder 15 drives first
Electromagnet 29 gradually does retract action, and the unmanned plane power battery 3 in battery mounting base 22 is due to by magnetic pulling force, electricity at this time
Pond out splice going splice 1 starts to be detached from the power interface 12 of 22 inside of battery mounting base, and unmanned plane power battery 3 is with the first electromagnetism
Iron 29 is together in retraction movement to battery placing groove 30, and unmanned plane unit 11 has completed battery roll process at this time；
Further, driving device driving unmanned plane rests frame 28 and rotates horizontally, and skids off the battery of battery mounting base 22
22.1 rotation of end is extremely towards the ejection opening 3.2 of battery ejection case 27；The second electromagnet 26 is powered, and then second by moment at this time
Battery iron 26 generates strong row with 3.1 moment of the second permanent magnet in battery ejection case 27 on top layer's unmanned plane power battery 3
Repulsion, so battery ejection case 27 in top layer's unmanned plane power battery 3 repulsive force effect under by rapidly from ejection opening 3.2
Ejection is gone out, ejection process once occur the second electromagnet 26 is powered off immediately, battery ejection case 27 in the former second layer nobody
Mechanomotive force battery 3 spring 46 effect under move up to it is equal with the second electromagnet 26, preparation launched again, ejected
The unmanned plane power battery 3 gone slides to battery mounting base 22 under the guiding function of battery guiding channel 32, logical from battery guiding
The battery of unmanned plane power battery 3 from battery mounting base 22 that road 32 skids off skids off end 22.1 and is slipped into battery mounting base 22,
And the battery out splice going splice 1 of unmanned plane power battery 3 corresponds to insertion 22 upper power source interface 12 of battery mounting base under effect of inertia
In, 19 automatic magnetic of the first permanent magnet connects the magnetic component of the upside of the unmanned plane power battery 3, the magnetic component at this time
Magnetic attraction much smaller than repulsive force between the second battery iron 26 and the second permanent magnet 3.1, further prevent unmanned plane power electric
It is skidded off automatically in 3 flight course of pond, realizes the installation process of battery；Then the chuck of four scroll chucks 14 of driving is electric simultaneously
Machine 17 makes it be totally released four to rest support feet 10, finally unmanned plane unit is driven to take off vertically.
The above is only the preferred embodiment of the present invention, it should be pointed out that：For the ordinary skill people of the art
For member, various improvements and modifications may be made without departing from the principle of the present invention, these improvements and modifications also should
It is considered as protection scope of the present invention.
Claims (9)
1. a kind of unmanned plane relay station, it is characterised in that：Including relay station ontology (18), unmanned plane unit (11), unmanned electromechanics
Pond removable unit and unmanned machine battery installation unit；
The unmanned plane unit (11), which is rested, to be installed at the top of the relay station car body (18)；On the relay station car body (18) also
It is provided with unmanned plane battery roll unit and unmanned machine battery installation unit, the unmanned plane battery roll unit and unmanned electromechanics
Pond installation unit is located at side before and after the unmanned plane unit (11) of resting state respectively.
2. a kind of unmanned plane relay station according to claim 1, it is characterised in that：Relay station ontology (18) top water
The flat unmanned plane that is provided with rests frame (28), and driving device, which can drive, rests frame (28) horizontal rotation；The unmanned plane unit (11)
It rests and is installed on the unmanned plane and rests on frame (28)；
Battery mounting base (22) is provided on the downside of the unmanned plane unit (11), unmanned plane power battery (3) is slided from side level
Enter to be installed in the battery mounting base (22), and the end of slipping into of unmanned plane power battery (3) is provided with battery out splice going splice
(1), the battery out splice going splice (1) is corresponding is inserted into the power interface (12) on the inside of the battery mounting base (22)；Rotation institute
State unmanned plane rest frame (28) can drive the battery of battery mounting base (22) skid off end (22.1) rotate successively to respectively with nobody
Machine battery removable unit and unmanned machine battery installation unit correspond to.
3. a kind of unmanned plane relay station according to claim 2, it is characterised in that：Four of the unmanned plane unit (11)
Support feet (10) of resting is arranged to cylinder；The unmanned plane rests frame (28) in decussation structure, and the unmanned plane stops
Have a rest frame (28) quadrangle on the upside of be separately installed with four scroll chucks (14)；It rests described in four of the unmanned plane unit (11)
The concentric correspondence of support feet (10) difference is in four scroll chucks (14)；Each scroll chuck (14) can clamp or pine
Open the corresponding support feet (10) of resting.
4. a kind of unmanned plane relay station according to claim 3, it is characterised in that：The unmanned plane power battery (3)
Both sides are provided with draw runner (2) along its length；Draw runner guide groove (43), two cunnings are provided on the battery mounting base (22)
Item (2) is slideably positioned in respectively in the corresponding draw runner guide groove (43)；The upside setting of the unmanned plane power battery (3)
There is magnetic component；It is provided in the battery mounting base (22) and corresponding first permanent magnet of unmanned plane power battery (3)
(19), the first permanent magnet (19) magnetic connects the magnetic component of the upside of the unmanned plane power battery (3).
5. a kind of unmanned plane relay station according to claim 4, it is characterised in that：The unmanned plane rests on frame (28) also
It is installed with ejection guiding device (25)；The ejection guiding device (25) is the box structure penetrated through along its length, the bullet
It penetrates on the inside of guiding device (25) as battery guiding channel (32)；
The battery guiding channel (32) skids off end (22.1) with the battery of the battery mounting base (22) and docks setting；From described
Unmanned plane power battery (3) correspondence skidded off in battery mounting base (22) is slipped into the battery guiding channel (32)；The electricity
Guiding channel (32) two madial wall upper edge battery in pond skids off direction and has been extended draw runner guiding groove (33), unmanned plane power battery
(3) two draw runners (2) on are correspondingly arranged respectively with the two draw runner guiding grooves (33).
6. a kind of unmanned plane relay station according to claim 4, it is characterised in that：Unmanned plane power battery (3) is installed on
In the battery mounting base (22) under state, the unmanned plane power battery (3) is close to the battery of the battery mounting base (22)
It skids off end (22.1) side and is provided with the second permanent magnet (3.1).
7. a kind of unmanned plane relay station according to claim 6, it is characterised in that：The unmanned plane battery roll unit packet
Include dismounting platform (30.1)；The front and rear electromagnetism placing groove (30) penetrated through of setting, the battery are put on the dismounting platform (30.1)
It puts the one end of slot (30) far from the unmanned plane unit (11) and is provided with cylinder block (16), the cylinder block (16) is close to the nothing
One end of man-machine unit (11) is provided with telescopic cylinder (15), and the telescopic cylinder (15) is front and rear along the battery placing groove (30)
Direction extension is penetrated through, telescopic cylinder (15) end is provided with the first electromagnet (29), and the telescopic cylinder (15) can drive
First electromagnet (29) is extend out at the battery mounting base (22) of unmanned plane unit (11), and telescopic cylinder (15) can also drive first
Electromagnet (29) is retracted in battery placing groove (30)；Under first electromagnet (29) energized state, the first electromagnet (29)
With the second permanent magnet (3.1) mutual magnetic in the battery mounting base (22) on unmanned plane power battery (3).
8. a kind of unmanned plane relay station according to claim 6, it is characterised in that：The unmanned machine battery installation unit packet
Include battery ejection case (27), the second electromagnet (26) and the second electromagnet fixed seat (45)；
The battery ejection case (27) is body structure；The intracavity bottom of the battery ejection case (27) is provided with longitudinal spring
(46), several unmanned plane power batteries (3) for stacking setting of the upper end top pressure of the longitudinal spring (46)；
Second electromagnet (26) is fixedly installed in the battery by the second electromagnet fixed seat (45) and launches case (27) outside
Side, and second electromagnet (26) is positioned at side of the battery ejection case (27) far from the unmanned plane unit (11)；Institute
It states battery ejection case (27) and offers ejection opening (3.2), the ejection close to the side upper end of the unmanned plane unit (11)
Opening (3.2) is correspondingly arranged with second electromagnet (26)；Under second electromagnet (26) energized state, the second electromagnet (26)
Mutually exclusive, the battery with the second permanent magnet (3.1) in battery ejection case (27) on top layer's unmanned plane power battery (3)
Launching top layer's unmanned plane power battery (3) in case (27) can be through in ejection opening (3.2) pop-up to battery guiding channel (32).
9. according to a kind of method of unmanned plane relay station of any one of claim 1 to 8, it is characterised in that：
During unmanned plane during flying state, stop the serious forgiveness of pick-up point to ensure that its unmanned plane unit (11) makes a return voyage, each scroll chuck
(14) chuck motor (17) driving radially movable to the maximum open configuration of movable jaw, normally flies in unmanned plane unit (11)
During row, when the electricity of entrained unmanned plane power battery (3) will exhaust, at this moment controller controls unmanned plane unit (11)
It makes a return voyage, the unmanned plane unit (11) of flight is gradually flown to right over relay station ontology (18), controls the unmanned plane list of flight at this time
First (11) slow vertical landing, until four of unmanned plane unit (11) rest support feet (10) and stretch into corresponding four openings shape
In the scroll chuck (14) of state, unmanned plane unit has been completed to land at this time, starts one of scroll chuck (14) at this time
Chuck motor (17) makes three movable jaws of its single scroll chuck (14) do pinching action radially inward, treats to press from both sides completely
Support feet (10) of tightly resting is suspended before to be continued to clamp, and is driven the chuck motor (17) of second scroll chuck (14) at this time, is made
Three movable jaws of its second scroll chuck (14) do pinching action radially inward, treat to clamp completely and rest support feet
(10) pause continues to clamp before；Unmanned plane unit (11) is basically completed positioning at this time, successively will continue in this way at this time
Third, the 4th scroll chuck (14) chuck motor (17) and do pinching action；Then four scroll chucks are driven simultaneously
(14) chuck motor (17) makes it clamp four completely respectively to rest support feet (10), and unmanned plane unit (11) is complete at this time
Full unmanned plane is positioned to rest on frame (28)；
At this time driving device driving unmanned plane rest frame (28) horizontal rotation, the battery of battery mounting base (22) is made to skid off end
(22.1) rotation drives telescopic cylinder (15) that the first electromagnet (29) is driven to extend out to nothing at this time to towards dismounting platform (30.1)
The battery of the battery mounting base (22) of man-machine unit (11) is skidded off at end (22.1), is then powered to the first electromagnet (29), this
When the first electromagnet (29) second permanent magnet (3.1) in battery mounting base (22) on unmanned plane power battery (3) mutually inhale
Draw；Then driving telescopic cylinder (15) drives the first electromagnet (29) gradually to do retract action, at this time in battery mounting base (22)
Unmanned plane power battery (3) due to by magnetic pulling force, battery out splice going splice (1) starts to be detached from the inside of battery mounting base (22)
Power interface (12), and unmanned plane power battery (3) with the first electromagnet (29) together retraction movement to battery placing groove
(30) in, unmanned plane unit (11) has completed battery roll process at this time；
Further, driving device driving unmanned plane rest frame (28) horizontal rotation, skid off the battery of battery mounting base (22)
(22.1) rotation to the ejection towards battery ejection case (27) is held to be open (3.2)；The second electromagnet (26) is powered by moment at this time,
And then second the second permanent magnet on top layer's unmanned plane power battery (3) in battery iron (26) and battery ejection case (27)
(3.1) moment generates strong repulsive forces, and then top layer's unmanned plane power battery (3) is repelling masterpiece in battery ejection case (27)
It is launched away with lower from ejection opening (3.2) rapidly, ejection process once occurs immediately powering off the second electromagnet (26), electricity
Former second layer unmanned plane power battery (3) in pond ejection case (27) moves up to and the second electromagnetism under spring (46) effect
Iron (26) is equal, and preparation is launched again, by unmanned plane power battery (3) the drawing in battery guiding channel (32) that ejection is gone out
It leads and slides to battery mounting base (22) under effect, pacify from the unmanned plane power battery (3) that battery guiding channel (32) skids off from battery
The battery of dress seat (22) skids off end (22.1) and is slipped into battery mounting base (22), and the unmanned plane power battery under effect of inertia
(3) battery out splice going splice (1) is corresponding to be inserted into battery mounting base (22) upper power source interface (12), at this time the first permanent magnet (19)
Automatic magnetic connects the magnetic component of the upside of the unmanned plane power battery (3), and the magnetic attraction of the magnetic component is much smaller than the
Repulsive force between two battery iron (26) and the second permanent magnet (3.1) further prevents unmanned plane power battery (3) flight course
In skid off automatically, realize the installation process of battery；Then the chuck motor (17) of four scroll chucks (14) is driven to make simultaneously
It is totally released four and rests support feet (10), finally unmanned plane unit is driven to take off vertically.
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