CN108313320A - A kind of movable unmanned helicopter rests platform - Google Patents
A kind of movable unmanned helicopter rests platform Download PDFInfo
- Publication number
- CN108313320A CN108313320A CN201810122429.6A CN201810122429A CN108313320A CN 108313320 A CN108313320 A CN 108313320A CN 201810122429 A CN201810122429 A CN 201810122429A CN 108313320 A CN108313320 A CN 108313320A
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- battery
- unmanned plane
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- rests
- frame
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- 238000010248 power generation Methods 0.000 claims abstract description 13
- 238000009826 distribution Methods 0.000 claims abstract description 4
- 230000005540 biological transmission Effects 0.000 claims description 19
- 230000000284 resting effect Effects 0.000 claims description 13
- 238000009434 installation Methods 0.000 claims description 12
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 11
- 230000005611 electricity Effects 0.000 claims description 9
- 229910052742 iron Inorganic materials 0.000 claims description 5
- 230000001360 synchronised effect Effects 0.000 claims description 5
- 238000003780 insertion Methods 0.000 claims description 2
- 230000037431 insertion Effects 0.000 claims description 2
- 230000005389 magnetism Effects 0.000 claims 1
- 238000000034 method Methods 0.000 abstract description 7
- 230000000694 effects Effects 0.000 abstract description 6
- 238000010586 diagram Methods 0.000 description 5
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 241000237858 Gastropoda Species 0.000 description 1
- 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
- 238000011900 installation process Methods 0.000 description 1
- 230000001846 repelling effect Effects 0.000 description 1
Classifications
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- 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
- B60L8/00—Electric propulsion with power supply from forces of nature, e.g. sun or wind
- B60L8/003—Converting light into electric energy, e.g. by using photo-voltaic systems
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60P—VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TO CARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS
- B60P3/00—Vehicles adapted to transport, to carry or to comprise special loads or objects
- B60P3/06—Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles
- B60P3/11—Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles for carrying aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- 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
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
-
- 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
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
-
- 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
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Power Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Health & Medical Sciences (AREA)
- Public Health (AREA)
- Toys (AREA)
- Electric Propulsion And Braking For Vehicles (AREA)
Abstract
It includes mobile platform car body, wheel power battery, wheel electrical machine, wheel, solar power generation plate unit and drone body to rest platform the invention discloses a kind of movable unmanned helicopter；The four wheel power batteries are uniformly installed on the platform vehicle bottom at rectangular array, and four wheel electrical machines are drivingly connected with four wheels respectively；The four wheel power batteries are electrically connected with four wheel electrical machines respectively；The four solar panel unit horizontals are installed at the top of the mobile platform car body, and the four solar power generation plate unit rectangular array distributions, the electric energy output end of the four solar power generation plate units are connect with the four wheel power battery powereds respectively；The structure of the present invention is simple, and unmanned plane power battery is installed in the form of electromagnetic launch, has the characteristics that process is rapid, realizes the quickly main automatic effect for replacing battery.
Description
Technical field
Platform is rested the invention belongs to unmanned plane field more particularly to a kind of movable unmanned helicopter.
Background technology
There is the excellent performances such as light and handy, flexible, acceleration height by the unmanned plane of power of battery, 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 exhausting battery, it is therefore desirable to which a kind of movement that can replace battery rests platform.
Invention content
Goal of the invention：In order to overcome the deficiencies in the prior art, the present invention provide one kind can be unmanned plane automatically more
The movable unmanned helicopter for changing battery rests platform.
Technical solution：To achieve the above object, a kind of movable unmanned helicopter of the invention rests platform, including mobile platform
Car body, wheel power battery, wheel electrical machine, wheel, solar power generation plate unit and drone body；
The four wheel power batteries are uniformly installed on the platform vehicle bottom, the four wheel electricity at rectangular array
Machine is drivingly connected with four wheels respectively；The four wheel power batteries are electrically connected with four wheel electrical machines respectively；Described in four
Solar panel unit horizontal is installed at the top of the mobile platform car body, and the four solar power generation plate units are rectangular
The electric energy output end of array distribution, the four solar power generation plate units is connect with the four wheel power battery powereds respectively；
It is also horizontally disposed at the top of the mobile platform car body to there is unmanned plane to rest frame, and the unmanned plane rests frame and is located at four
The centre that the solar panels are enclosed；The drone body, which is rested, to be installed on the unmanned plane and rests on frame.
Further, the mobile platform car body bottom level, which is provided with, rests frame motor；Further include geared worm, transmission
Turbine and the frame transmission axis that rests；Frame motor and the geared worm of resting is drivingly connected, the geared worm with it is described
It is driven turbine drives connection；
The frame transmission vertical synchronized links of axis that rest rest in the unmanned plane on the downside of frame, rest frame biography described in rotation
Dynamic axis can make unmanned plane rest frame horizontal synchronization rotation；The concentric synchronized links of the transmission turbine are driven in the frame that rests
Axis lower end.
Further, rainhat is arranged in the unmanned plane body top, and each wing arm of the unmanned plane main body includes upper
Under upper and lower arms disposed in parallel, the extending end of wherein underarm is longer than the upper arm, and the upper and lower arms pass through several
Connecting pole is fixedly connected, and the spiral wing of wherein unmanned plane main body is installed on the underarm end；The plate of the upper and lower arms
Face hollow out has several structure holes.
Further, it is provided with battery mounting base on the downside of the drone body；
Further include battery case and battery body；The battery body is arranged in the battery holding tank of the battery case,
Described in battery body charging connector buckle be set in the charging connector placing groove on the inside of the battery case；
The battery case is slid horizontally into from side to be installed in the battery mounting base, the battery output of the battery body
Connector is fixedly installed on the slide-in end of the battery case, and battery out splice going splice slides into direction along battery case and corresponds to the insertion electricity
In power interface on the inside of the mounting base of pond；
The both sides of the battery case are provided with draw runner along its length；Draw runner is provided on the battery mounting base to lead
Slot, two draw runners are slideably positioned in respectively in the corresponding draw runner guide groove；It is provided with magnetic on the upside of the battery case
Component；The first permanent magnet corresponding with battery case, the first permanent magnet magnetic connection are provided in the battery mounting base
The magnetic component of the upside of the battery case.
Further, four of the drone body bottom rest support leg and are arranged to cylinder；The unmanned plane stops
Frame of having a rest be in decussation structure, the unmanned plane rest frame quadrangle on the upside of be separately installed with four scroll chucks；The nothing
Support leg of resting described in four of man-machine ontology distinguishes concentric correspondence in four scroll chucks；Each scroll chuck
It may tighten or loosen the corresponding support leg of resting.
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 the battery case that skids off correspond to and slide into the battery guiding channel；Two madial wall upper edge battery of the battery guiding channel skids off
Direction, which is extended, draw runner guiding groove, and two draw runners on battery case are correspondingly arranged with the two draw runner guiding grooves respectively.
Battery case is installed in the battery mounting base under state, battery of the battery case close to the battery mounting base
It skids off end side and is provided with the second permanent magnet.
Further, further include unmanned plane battery roll unit on the mobile platform car body, the unmanned machine battery is torn open
It unloads unit to be located on front side of the drone body, the unmanned plane, which rests frame, can drive the battery of battery mounting base to skid off end rotation
Extremely towards unmanned plane battery roll unit；
The unmanned plane battery roll unit includes dismounting platform；The front and back electromagnetism penetrated through is arranged on the dismounting platform to put
Slot is set, the described one end of battery placing groove far from the drone body is provided with cylinder block, and the cylinder block is close to the nothing
One end of man-machine ontology is provided with telescopic cylinder, and the telescopic cylinder penetrates through direction extension, institute before and after the battery placing groove
It states telescopic cylinder end and is provided with the first electromagnet, the telescopic cylinder can drive the first electromagnet to extend out to drone body
At battery mounting base, telescopic cylinder can also drive the first electromagnet to be retracted in battery placing groove；First electromagnet is powered
Under state, the first electromagnet and the mutual magnetic of the second permanent magnet on battery case in the battery mounting base.
Further, on the mobile platform car body further include unmanned machine battery installation unit；The unmanned machine battery peace
Dress unit is located on rear side of the drone body；The unmanned plane rest frame can drive the battery of battery mounting base skid off end rotation
To towards unmanned machine battery installation unit；
Unmanned machine battery installation unit includes battery ejection case, the second electromagnet and the second electromagnet fixed seat；The electricity
It is body structure that case is launched in pond；The intracavity bottom of the battery ejection case is provided with longitudinal spring, the upper end of the longitudinal spring
Several battery cases for stacking setting of top pressure；
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 drone body；The battery launches case close to the nothing
The side upper end of man-machine ontology offers ejection opening, and the ejection opening is correspondingly arranged with second electromagnet；Second electricity
Under magnet energized state, the second permanent magnet on the second electromagnet and battery ejection Xiang Zhong top layers battery case is mutually exclusive, institute
Stating battery ejection Xiang Zhong top layers battery case can be through in ejection opening pop-up to battery guiding channel.
Advantageous effect：The structure of the present invention is simple, rests in rotatable unmanned plane and triangle chuck is arranged on frame, structure makes
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 being installed in the form of electromagnetic launch, have the characteristics that process is rapid, realizes quick
The main automatic effect for replacing battery.
Description of the drawings
Attached drawing 1 is the whole front view of the present invention；
Attached drawing 2 is overall top view of the present invention；
Attached drawing 3 is the whole upward view of the present invention；
Attached drawing 4 is that battery launches partial sectional view at case；
Attached drawing 5 is unmanned plane battery roll the first schematic diagram of state；
Attached drawing 6 is unmanned plane battery roll the second schematic diagram of state；
Attached drawing 7 is the wing arm configuration schematic diagram of drone body；
Attached drawing 8 is battery body scheme of installation；
Attached drawing 9 is that unmanned plane rests frame schematic diagram；
Attached drawing 10 is the partial schematic diagram at the battery mounting base of drone body.
Specific implementation mode
The present invention is further described below in conjunction with the accompanying drawings.
The introduction about the construction of this programme：
A kind of movable unmanned helicopter as shown in attached drawing 1 to 10 rests platform, including mobile platform car body 18, wheel power
Battery 35, wheel electrical machine 38, wheel 40, solar power generation plate unit 23 and drone body 11；
The four wheel power batteries 35 are uniformly installed on 18 bottom of platform car body, four vehicles at rectangular array
Turbin generator 38 is drivingly connected with four wheels 40 respectively；The four wheel power batteries 35 are electrical with four wheel electrical machines 38 respectively
Connection；The four solar power generation plate units 23 are horizontally installed to 18 top of the mobile platform car body, and four solar energy
Generate electricity the distribution of 23 rectangular array of plate unit, the electric energy output ends of the four solar power generation plate units 23 respectively with four vehicles
Power battery 35 is taken turns for electrical connection；
The top of the mobile platform car body 18 is also horizontally disposed to have unmanned plane to rest frame 28, and the unmanned plane rests frame 28
Positioned at the centre that four solar panels 23 are enclosed；The drone body 11, which is rested, to be installed on the unmanned plane and rests
On frame 28.
18 bottom level of mobile platform car body, which is provided with, rests frame motor 31；Further include geared worm 36, transmission whirlpool
Wheel 41 and the frame transmission axis 41.1 that rests；The frame motor 31 that rests is drivingly connected with the geared worm 36, the transmission snail
Bar 36 is drivingly connected with the transmission turbine 41；
The frame transmission 41.1 vertical synchronized links of axis that rest rest the downside of frame 28 in the unmanned plane, stop described in rotation
Frame of having a rest transmission axis 41.1 can make unmanned plane rest 28 horizontal synchronization of frame rotation；The 41 concentric synchronized links of transmission turbine in
41.1 lower end of frame transmission axis of resting.
Rainhat 11.1 is arranged in 11 top of the unmanned plane main body, and each wing arm of the unmanned plane main body 11 includes up and down
The extending end of upper arm 7 and underarm 7.1 disposed in parallel, wherein underarm 7.1 is longer than the upper arm 7, the upper arm 7 and underarm
7.1 are fixedly connected by several connecting poles 9, and the spiral wing 7.2 of wherein unmanned plane main body 11 is installed on 7.1 end of the underarm
End；The plate face hollow out of the upper arm 7 and underarm 7.1 has several structure holes 8, and then reduces its unmanned plane weight.
11 downside of the drone body is provided with battery mounting base 22；
Further include battery case 3 and battery body 4；The battery body 4 is arranged in the battery holding tank of the battery case 3
In, it is set in the charging connector placing groove 5 of 3 inside of the battery case wherein the charging connector 6 of the battery body 4 buckles；
When needing to charge to it, it can be taken off charging connector 6 and charge；
The battery case 3 is slid horizontally into from side to be installed in the battery mounting base 22, the battery of the battery body 4
Out splice going splice 1 is fixedly installed on the slide-in end 3.1 of the battery case 3, and battery out splice going splice 1 slides into direction along battery case and corresponds to
It is inserted into the power interface 12 of 22 inside of the battery mounting base；
The both sides of the battery case 3 are provided with draw runner 2 along its length；It is provided with draw runner on the battery mounting base 22
Guide groove 43, two draw runners 2 are slideably positioned in respectively in the corresponding draw runner guide groove 43；The upside of the battery case 3 is set
It is equipped with magnetic component；First permanent magnet 19 corresponding with battery case 3 is provided in the battery mounting base 22, described first forever
19 magnetic of magnet connects the magnetic component of the upside of the battery case 3.
Four of 11 bottom of the drone body rest support leg 10 and are arranged to cylinder；The unmanned plane rests frame 28
In decussation structure, the unmanned plane rest frame 28 quadrangle on the upside of be separately installed with four scroll chucks 14；The nothing
Support leg 10 of resting described in four of man-machine ontology 11 distinguishes concentric correspondence in four scroll chucks 14；Each described three
Dog chuck 14 may tighten or loosen the corresponding support leg 10 of resting.
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 the 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 battery case 3 skidded off in pond mounting base 22, which corresponds to, to be slid into the battery guiding channel 32；In 32 liang of the battery guiding channel
Side wall upper edge battery skid off direction be extended have draw runner guiding groove 33, two draw runners 2 on battery case 3 respectively with two draw runners
Guiding groove 33 is correspondingly arranged.
Battery case 3 is installed in the battery mounting base 22 under state, and the battery case 3 is close to the battery mounting base 22
Battery skid off end 22.1 sides be provided with the second permanent magnet 3.1.
Further include unmanned plane battery roll unit, the unmanned plane battery roll unit position on the mobile platform car body 18
In the front side of the drone body 11, the unmanned plane, which rests frame 28, can drive the battery of battery mounting base 22 to skid off 22.1 rotation of end
It goes to towards unmanned plane battery roll unit；
The unmanned plane battery roll unit includes dismounting platform 30.1；Front and back perforation is set on the dismounting platform 30.1
Electromagnetism placing groove 30,30 one end far from the drone body 11 of the battery placing groove is provided with cylinder block 16, described
Cylinder block 16 is provided with telescopic cylinder 15 close to one end of the drone body 11, and the telescopic cylinder 15 is put along the battery
It sets the front and back perforation direction of slot 30 to extend, 15 end of the telescopic cylinder is provided with the first electromagnet 29, and the telescopic cylinder 15 can
The first electromagnet 29 is driven to extend out at the battery mounting base 22 of drone body 11, telescopic cylinder 15 can also drive the first electromagnetism
Iron 29 is retracted in battery placing groove 30；Under first electromagnet, 29 energized state, the first electromagnet 29 is pacified with the battery
Fill the 3.1 mutual magnetic of the second permanent magnet on battery case 3 in seat 22.
It further include unmanned machine battery installation unit on the mobile platform car body 18；The unmanned machine battery installation unit position
In 11 rear side of the drone body；The unmanned plane rest frame 28 can drive the battery of battery mounting base 22 skid off end 22.1 rotation
It goes to towards unmanned machine battery installation unit；
Unmanned machine battery installation unit includes 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, described vertical
To several battery cases 3 for stacking setting of upper end top pressure of 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 drone body 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 drone body 11
Electromagnet 26 is correspondingly arranged；Under second electromagnet, 26 energized state, the second electromagnet 26 and top layer's electricity in battery ejection case 27
The second permanent magnet 3.1 on pond shell 3 is mutually exclusive, and top layer's battery case 3 can be through ejection opening 3.2 in the battery ejection case 27
In pop-up to battery guiding channel 32.
The method, process, principle and technological progress of this programme arrange as follows：
When unmanned plane during flying state, in order to ensure that its drone body 11 " making a return voyage " stops the serious forgiveness of pick-up point, each three-jaw
The chuck motor 17 of chuck 14 drives radially movable to the maximum open configuration of movable jaw, in 11 normal flight of drone body
In the process, when the electricity of entrained battery case 3 will exhaust, at this moment controller control drone body 11 is maked a return voyage, the nothing of flight
Man-machine ontology 11 is gradually flown to right over middle mobile platform car body 18, and the drone body 11 for controlling flight at this time slowly vertically drops
It falls, until four of drone body 11 rest support leg 10 and stretch into the scroll chuck 14 of corresponding four open configurations, this
When drone body completed to land, start the chuck motor 17 of one of scroll chuck 14 at this time, make its single three-jaw
Three movable jaws of chuck 14 do pinching action radially inward, wait for clamping completely resting to suspend before support leg 10 and continue to press from both sides
Tightly, the chuck motor 17 for driving second scroll chuck 14 at this time, makes three movable jaw edges of its second scroll chuck 14
Pinching action is radially-inwardly done, waits for clamping completely resting to suspend before support leg 10 and continues to clamp；11 base of drone body at this time
This completion positions, continue in this way at this time successively by third, the 4th scroll chuck 14 chuck motor 17 and press from both sides
Tight 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 leg
10, at this time drone body 11 be fully positioned at unmanned plane and rested on frame 28；
At this time driving device driving unmanned plane rest frame 28 horizontal rotation, so that the battery of battery mounting base 22 is skidded off end 22.1
Rotation drives telescopic cylinder 15 that the first electromagnet 29 is driven to extend out to drone body 11 at this time to towards dismounting platform 30.1
The battery of battery mounting base 22 skids off at end 22.1, then the first electromagnet 29 is given to be powered, the first electromagnet 29 is in battery at this time
The second permanent magnet 3.1 in mounting base 22 on battery case 3 attracts each other；Then driving telescopic cylinder 15 drives the first electromagnet 29
Retract action gradually is done, the battery case 3 in battery mounting base 22 is since by magnetic pulling force, battery out splice going splice 1 starts at this time
Be detached from the power interface 12 of the inside of battery mounting base 22, and battery case 3 with the first electromagnet 29 together retraction movement to battery
In placing groove 30, drone body 11 has completed battery roll process at this time；
Further, driving device driving unmanned plane rest frame 28 horizontal rotation, so that the battery of battery mounting base 22 is skidded off
The ejection opening 3.2 of case 27 is extremely launched in 22.1 rotation of end towards battery；The second electromagnet 26 is powered by moment at this time, and then second
Battery iron 26 generates strong repulsive forces with 3.1 moment of the second permanent magnet in battery ejection case 27 on top layer's battery case 3, in turn
Top layer's battery case 3 is launched away from ejection opening 3.2 rapidly in the case where repelling force effect in battery ejection case 27, ejection process
Once appearance immediately powers off the second electromagnet 26, battery launches the former second layer battery case 3 in case 27 under the effect of spring 46
Move up to it is equal with the second electromagnet 26, preparation launched again, the battery case 3 gone out by ejection is in battery guiding channel
Battery mounting base 22 is slided under 32 guiding function, the battery case 3 skidded off from battery guiding channel 32 is from battery mounting base 22
Battery skids off end 22.1 and slides into battery mounting base 22, and the correspondence of battery out splice going splice 1 of battery case 3 is inserted under effect of inertia
Enter in 22 upper power source interface 12 of battery mounting base, 19 automatic magnetic of the first permanent magnet connects the upside of the battery case 3 at this time
Magnetic component, the magnetic attraction of the magnetic component is much smaller than between the second battery iron 26 and the second permanent magnet 3.1 in the present embodiment
Repulsive force further prevents skidding off automatically in 3 flight course of battery case, realizes the installation process of battery；Then it drives simultaneously
The chuck motor 17 of four scroll chucks 14 makes it be totally released four to rest support leg 10, finally drive drone body vertical
It takes off.
Remarks, magnetic between electromagnet and permanent magnet and repulsion in this implementation are utilized opposite pole and attract each other,
The mutually exclusive principle of like pole.
The above is only a 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 are also answered
It is considered as protection scope of the present invention.
Claims (8)
1. a kind of movable unmanned helicopter rests platform, it is characterised in that：Including mobile platform car body (18), wheel power battery
(35), wheel electrical machine (38), wheel (40), solar power generation plate unit (23) and drone body (11)；
The four wheel power batteries (35) are uniformly installed on platform car body (18) bottom, four vehicles at rectangular array
Turbin generator (38) is drivingly connected with four wheels (40) respectively；The four wheel power batteries (35) respectively with four wheel electrical machines
(38) it is electrically connected；The four solar power generation plate units (23) are horizontally installed at the top of the mobile platform car body (18), and
Four solar power generation plate unit (23) the rectangular array distributions, the electric energy output of the four solar power generation plate units (23)
End is respectively with the four wheel power batteries (35) for being electrically connected；
It is also horizontally disposed at the top of the mobile platform car body (18) to there is unmanned plane to rest frame (28), and the unmanned plane rests frame
(28) it is located at the centre that four solar panels (23) are enclosed；The drone body (11), which is rested, is installed on the nothing
It is man-machine to rest on frame (28).
2. a kind of movable unmanned helicopter according to claim 1 rests platform, it is characterised in that：The mobile platform car body
(18) bottom level, which is provided with, rests frame motor (31)；Further include geared worm (36), transmission turbine (41) and the frame that rests transmission
Axis (41.1)；The frame motor (31) that rests is drivingly connected with the geared worm (36), the geared worm (36) and institute
Transmission turbine (41) is stated to be drivingly connected；
The vertical synchronized links of frame transmission axis (41.1) that rest rest in the unmanned plane on the downside of frame (28), stop described in rotation
Frame of having a rest transmission axis (41.1) can make unmanned plane rest frame (28) horizontal synchronization rotation；The concentric synchronization of the transmission turbine (41)
It is connected to described frame transmission axis (41.1) lower end of resting.
3. a kind of movable unmanned helicopter according to claim 1 rests platform, it is characterised in that：The unmanned plane main body
(11) each wing arm of top setting rainhat (11.1), the unmanned plane main body (11) includes upper and lower upper arm disposed in parallel
(7) and underarm (7.1), the extending end of wherein underarm (7.1) are longer than the upper arm (7), the upper arm (7) and underarm (7.1)
It is fixedly connected by several connecting poles (9), the spiral wing (7.2) of wherein unmanned plane main body (11) is installed on the underarm
(7.1) end；The plate face hollow out of the upper arm (7) and underarm (7.1) has several structure holes (8).
4. a kind of movable unmanned helicopter according to claim 2 rests platform, it is characterised in that：The drone body
(11) downside is provided with battery mounting base (22)；
Further include battery case (3) and battery body (4)；The battery that the battery body (4) is arranged in the battery case (3) accommodates
In slot, wherein the charging connector that charging connector (6) buckle of the battery body (4) is set on the inside of the battery case (3) is put
It sets in slot (5)；
The battery case (3) is slid horizontally into from side to be installed in the battery mounting base (22), the electricity of the battery body (4)
Pond out splice going splice (1) is fixedly installed on the slide-in end (3.1) of the battery case (3), and battery out splice going splice (1) is slided along battery case
Enter in the power interface (12) that direction corresponds on the inside of the insertion battery mounting base (22)；
The both sides of the battery case (3) are provided with draw runner (2) along its length；It is provided with cunning on the battery mounting base (22)
Guide groove (43), two draw runners (2) are slideably positioned in respectively in the corresponding draw runner guide groove (43)；The battery case
(3) magnetic component is provided on the upside of；It is provided with the first permanent magnetism corresponding with battery case (3) in the battery mounting base (22)
Body (19), the first permanent magnet (19) magnetic connect the magnetic component of the upside of the battery case (3).
5. a kind of movable unmanned helicopter according to claim 4 rests platform, it is characterised in that：The drone body
(11) four of bottom rest support leg (10) and are arranged to cylinder；The unmanned plane rests frame (28) in decussation knot
Structure, the unmanned plane rest frame (28) quadrangle on the upside of be separately installed with four scroll chucks (14)；The drone body
(11) the concentric correspondence of support leg (10) of resting described in four difference is in four scroll chucks (14)；Each three-jaw
Chuck (14) may tighten or loosen the corresponding support leg (10) of resting.
6. a kind of movable unmanned helicopter according to claim 5 rests platform, it is characterised in that：The unmanned plane rests frame
(28) ejection guiding device (25) is also installed on；The ejection guiding device (25) is the box-shaped knot penetrated through along its length
Structure, ejection guiding device (25) inside 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 described
In the corresponding slide-in battery guiding channel (32) of battery case (3) skidded off in battery mounting base (22)；The battery guiding is logical
(32) two madial wall upper edge battery of road, which skids off direction and is extended, draw runner guiding groove (33), two draw runners (2) on battery case (3)
It is correspondingly arranged respectively with the two draw runner guiding grooves (33).
Battery case (3) is installed in the battery mounting base (22) under state, and the battery case (3) is close to the battery mounting base
(22) battery skids off end (22.1) side and is provided with the second permanent magnet (3.1).
7. a kind of movable unmanned helicopter according to claim 6 rests platform, it is characterised in that：The mobile platform car body
(18) further include unmanned plane battery roll unit on, before the unmanned plane battery roll unit is located at the drone body (11)
Side, the unmanned plane, which rests frame (28), can drive the battery of battery mounting base (22) to skid off end (22.1) rotation to towards unmanned plane
Battery roll unit；
The unmanned plane battery roll unit includes dismounting platform (30.1)；Front and back perforation is set on the dismounting platform (30.1)
Electromagnetism placing groove (30), the battery placing groove (30) is provided with cylinder block far from one end of the drone body (11)
(16), the cylinder block (16) is provided with telescopic cylinder (15), the flexible gas close to one end of the drone body (11)
Cylinder (15) extends along the front and back perforation direction of the battery placing groove (30), and telescopic cylinder (15) end is provided with the first electromagnetism
Iron (29), the telescopic cylinder (15) can drive the first electromagnet (29) to extend out to the battery mounting bases of drone body (11)
(22) at, telescopic cylinder (15) can also drive the first electromagnet (29) to be retracted in battery placing groove (30)；First electromagnetism
Under iron (29) energized state, the first electromagnet (29) and the second permanent magnet on battery case (3) in the battery mounting base (22)
(3.1) mutual magnetic.
8. a kind of movable unmanned helicopter according to claim 6 rests platform, it is characterised in that：The mobile platform car body
(18) further include unmanned machine battery installation unit on；After the unmanned machine battery installation unit is located at the drone body (11)
Side；The unmanned plane, which rests frame (28), can drive the battery of battery mounting base (22) to skid off end (22.1) rotation to towards unmanned plane
Battery installation unit；
Unmanned machine battery installation unit includes 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 battery cases (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 located at side of the battery ejection case (27) far from the drone body (11)；Institute
It states battery ejection case (27) and offers ejection opening (3.2), the ejection close to the side upper end of the drone body (11)
Opening (3.2) is correspondingly arranged with second electromagnet (26)；Under second electromagnet (26) energized state, the second electromagnet (26)
Mutually exclusive with the second permanent magnet (3.1) in battery ejection case (27) on top layer's battery case (3), the battery launches case
(27) top layer's battery case (3) can be through in ejection opening (3.2) pop-up to battery guiding channel (32) in.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810122429.6A CN108313320B (en) | 2018-02-07 | 2018-02-07 | Mobile unmanned aerial vehicle stopping platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810122429.6A CN108313320B (en) | 2018-02-07 | 2018-02-07 | Mobile unmanned aerial vehicle stopping platform |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108313320A true CN108313320A (en) | 2018-07-24 |
| CN108313320B CN108313320B (en) | 2023-06-23 |
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ID=62903731
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810122429.6A Active CN108313320B (en) | 2018-02-07 | 2018-02-07 | Mobile unmanned aerial vehicle stopping platform |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN110697059A (en) * | 2019-10-22 | 2020-01-17 | 国网安徽省电力有限公司蚌埠供电公司 | Unmanned aerial vehicle battery dismouting cabin |
| CN112278276A (en) * | 2020-11-12 | 2021-01-29 | 重庆凯创荣智能科技有限公司 | Battery replacing structure for unmanned aerial vehicle and using method of battery replacing structure |
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| WO2015135523A1 (en) * | 2014-03-13 | 2015-09-17 | Gassmann Uwe | Approach control for battery-operated flying devices |
| CN106828256A (en) * | 2017-03-10 | 2017-06-13 | 山东交通学院 | A kind of multifunctional traffic command car of supporting unmanned plane |
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| Publication number | Publication date |
|---|---|
| CN108313320B (en) | 2023-06-23 |
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Effective date of registration: 20240221 Address after: 230000 B-2704, wo Yuan Garden, 81 Ganquan Road, Shushan District, Hefei, Anhui. Patentee after: HEFEI LONGZHI ELECTROMECHANICAL TECHNOLOGY Co.,Ltd. Country or region after: China Address before: No.2 Xuefu Middle Road, Weiyang District, Xi'an City, Shaanxi Province, 720021 Patentee before: XI'AN TECHNOLOGICAL University Country or region before: China |