CN105752340B - Unmanned vehicle - Google Patents
Unmanned vehicle Download PDFInfo
- Publication number
- CN105752340B CN105752340B CN201610214440.6A CN201610214440A CN105752340B CN 105752340 B CN105752340 B CN 105752340B CN 201610214440 A CN201610214440 A CN 201610214440A CN 105752340 B CN105752340 B CN 105752340B
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- module
- medicine
- unmanned vehicle
- chest
- frame
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- 238000001802 infusion Methods 0.000 claims description 6
- 230000002572 peristaltic effect Effects 0.000 claims description 5
- 238000005507 spraying Methods 0.000 claims description 4
- 229920000049 Carbon (fiber) Polymers 0.000 claims 1
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- 230000032258 transport Effects 0.000 claims 1
- 230000005484 gravity Effects 0.000 abstract description 12
- 238000004806 packaging method and process Methods 0.000 abstract description 5
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- 239000007921 spray Substances 0.000 description 11
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- 238000004891 communication Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000009313 farming Methods 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
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- 230000002787 reinforcement Effects 0.000 description 2
- 238000003860 storage Methods 0.000 description 2
- 241000826860 Trapezium Species 0.000 description 1
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- 229940079593 drug Drugs 0.000 description 1
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Classifications
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- 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
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/16—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting
- B64D1/18—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting by spraying, e.g. insecticides
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- 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
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Life Sciences & Earth Sciences (AREA)
- Pest Control & Pesticides (AREA)
- Catching Or Destruction (AREA)
Abstract
Include the invention discloses a kind of unmanned vehicle：Fuselage, the fuselage has head and frame；Multiple horns, the multiple horn is provided at circumferentially spaced around the fuselage；Battery modules, the battery modules are detachably arranged in the frame；Medicine-chest module, the medicine-chest module is detachably arranged in the frame and the medicine-chest module is located between the head and the battery modules；Shower nozzle module, the shower nozzle module is located at least a portion of the multiple horn and is connected with the medicine-chest module；Pump housing module, the pump housing module is located on the fuselage and below the head；Electric mode transfer group, the electric mode transfer group is located on the fuselage and below the head.Unmanned vehicle packaging efficiency according to embodiments of the present invention is high, and position of centre of gravity is relatively stablized, having a smooth flight property.
Description
Technical field
Present invention relates particularly to a kind of unmanned vehicle.
Background technology
For the agriculture unmanned vehicle for managing, spraying insecticide for agro-farming, typically all can on the fuselage of aircraft
Be provided for depositing the medicine-chest of decoction, aircraft during flight, decoction in medicine-chest by spray dress be sprayed to it is to be painted
The areas such as farmland, the forest farm of medicine.With continuing for sprinkling process, amount of liquid medicine is gradually decreased, so that under the weight meeting constantly of medicine-chest
Drop, thus can attract the change of the position of centre of gravity of aircraft, so as to influence the flight of aircraft.
Moreover, the unmanned vehicle in correlation technique, due to the limitation of structure, the installation and removal of medicine-chest and battery are very
Inconvenience, so as to extend the time of assembly and disassembly.
The content of the invention
It is contemplated that at least solving one of technical problem in correlation technique to a certain extent.Therefore, the present invention is carried
Go out a kind of unmanned vehicle, the unmanned vehicle packaging efficiency is high, position of centre of gravity is relatively stablized, having a smooth flight property.
Unmanned vehicle according to embodiments of the present invention includes：Fuselage, the fuselage has head, the rear end of the head
Provided with frame；Multiple horns, the multiple horn is provided at circumferentially spaced around the fuselage；Battery mould for providing power
Group, the battery modules are detachably arranged in the frame；Medicine-chest module for storing decoction, the medicine-chest module is removable
It is located at unloading in the frame and the medicine-chest module is located between the head and the battery modules；For spraying decoction
Shower nozzle module, the shower nozzle module is located at least a portion of the multiple horn and is connected with the medicine-chest module；For
Decoction in the medicine-chest module is pumped into the pump housing module in the shower nozzle module, the pump housing module is located on the fuselage
And below the head；For the electric mode transfer group of automatically controlled regulation, the electric mode transfer group is located on the fuselage and positioned at institute
State below head.
Unmanned vehicle according to embodiments of the present invention, by by battery modules and medicine-chest module carry out modularized design and
Removably it is connected between frame, so as to so that the installation and removal of battery modules and medicine-chest module are easier to be quick,
The packaging efficiency of unmanned vehicle is improved, operating efficiency is improved.In addition, by the way that medicine-chest module is arranged on into head and battery
Between module, so that when medicine-chest module with the liquid level change of decoction when occurring mass change, because medicine-chest module is in
The middle part of fuselage, so that the position of centre of gravity of unmanned vehicle is relatively stablized, it is ensured that the having a smooth flight property of unmanned vehicle.
In some preferred embodiments, the battery modules are provided with limiting section, and the limiting section support is pressed in the medicine-chest
To limit the free degree that the medicine-chest module is moved upwards on module.
In some preferred embodiments, the battery modules include multiple batteries and battery case, the multiple battery
Core is integrated in the battery case, and the battery case is slidably disposed in the frame in the vertical direction.
In some preferred embodiments, one in the battery case and the frame is provided with chute and another
Provided with the slide rail slidably coordinated with the chute.
In some preferred embodiments, the electrical connection of mutual cooperation is respectively equipped with the frame and the battery case
Part, the electrical connector after battery modules are installed in place on the battery case and the electrical connector pair in the frame
Connect.
In some preferred embodiments, the medicine-chest module is slidably disposed in the frame in the vertical direction.
In some preferred embodiments, the frame is provided with brace rod, and the medicine-chest module is provided with multiple opening courts
Under neck, the multiple neck is respectively supported on the brace rod.
In some preferred embodiments, the medicine-chest module includes casing and the case lid being located on the casing, the case
Each in the relative two side wall of lid is equipped with multiple lug bosses, lower surface of the neck formation in the lug boss
On.
In some preferred embodiments, the shower nozzle module include it is multiple, and the pump housing module include multiple liquid pumps and
Pump housing shell, the multiple liquid pump is connected respectively with the multiple shower nozzle module by infusion channel and the multiple liquid pump is located at
In the pump housing shell, the pump housing shell is detachably arranged on the fuselage.
In some preferred embodiments, the quantity of the shower nozzle module is identical and the multiple with the quantity of the horn
Shower nozzle module is detachably arranged in the bottom of the end of the multiple horn respectively.
In some preferred embodiments, the unmanned vehicle also includes the difference module for being used to receiving and sending signal,
The difference module is located on the horn.
In some preferred embodiments, the unmanned vehicle also includes mounting bracket, and the difference module is located at described
In mounting bracket, the mounting bracket is detachably arranged on the horn by yoke configurations.
In some preferred embodiments, the shower nozzle module is connected through a screw thread structure and is located on the corresponding horn.
In some preferred embodiments, the unmanned vehicle also includes foot stool module, and the foot stool module is removably
The bottom of the head is located at, the foot stool module includes at least one foot stool, wherein the foot stool is by carbon fibre material system
Into slat element.
In some preferred embodiments, the unmanned vehicle also includes drain pan, and the drain pan is located at the pump housing mould
Outside group and the electric mode transfer group.
The additional aspect and advantage of the present invention will be set forth in part in the description, and will partly become from the following description
Obtain substantially, or recognized by the practice of the present invention.
Brief description of the drawings
The above-mentioned and/or additional aspect and advantage of the present invention will become from description of the accompanying drawings below to embodiment is combined
Substantially and be readily appreciated that, wherein：
Fig. 1 is the stereogram of unmanned vehicle according to embodiments of the present invention；
Fig. 2 is the enlarged drawing of a-quadrant in Fig. 1；
Fig. 3 is the top view of the unmanned vehicle shown in Fig. 1；
Fig. 4 is the front view of the unmanned vehicle shown in Fig. 1.
Reference：
Unmanned vehicle 100；
Fuselage 1；Head 11；Frame 12；Brace rod 121；
Horn 2；
Battery modules 3；Battery case 31；Limiting section 32；
Medicine-chest module 4；Casing 41；Case lid 42；Lug boss 421；Spiral cover 422；Handle 423；
Shower nozzle module 5；Shell 51；Spray disk 52；
Difference module 7；Mounting bracket 8；Yoke configurations 81；
Foot stool 10；Rotor 20；Motor 30, drain pan 40.
Embodiment
Embodiments of the invention are described below in detail, the example of the embodiment is shown in the drawings, wherein from beginning to end
Same or similar label represents same or similar element or the element with same or like function.Below with reference to attached
The embodiment of figure description is exemplary, is only used for explaining the present invention, and is not considered as limiting the invention.
In the description of the invention, it is to be understood that term " on ", " under ", "front", "rear", "left", "right", " perpendicular
Directly ", the orientation or position relationship of the instruction such as " level ", " top ", " bottom ", " interior ", " outer " are based on orientation shown in the drawings or position
Relation is put, the description present invention is for only for ease of and simplifies description, rather than indicate or imply that the device or element of meaning are necessary
With specific orientation, with specific azimuth configuration and operation, therefore it is not considered as limiting the invention.The present invention's
In description, " multiple " are meant that two or more, unless otherwise specifically defined.
In the description of the invention, it is necessary to illustrate, unless otherwise clearly defined and limited, term " installation ", " phase
Even ", " connection " should be interpreted broadly, for example, it may be being fixedly connected or being detachably connected, or be integrally connected；Can
To be mechanical connection or electrical connection；Can be joined directly together, can also be indirectly connected to by intermediary, Ke Yishi
The connection of two element internals or the interaction relationship of two elements.For the ordinary skill in the art, can be with
The concrete meaning of above-mentioned term in the present invention is understood as the case may be.
Unmanned vehicle 100 according to embodiments of the present invention is described below with reference to Fig. 1-Fig. 4.As Figure 1-Figure 4, according to
The unmanned vehicle 100 of the embodiment of the present invention includes：Fuselage 1, multiple horns 2, battery modules 3, medicine-chest module 4, shower nozzle module
5th, pump housing module (not shown) and electric mode transfer group (not shown).It is understood that according to embodiments of the present invention nobody
Aircraft 100 can be used in agro-farming industry carrying out the activities such as pesticide spraying to agricultural product.
Specifically, as Figure 1-Figure 4, fuselage 1 has head 11 and frame 12.Nobody can be provided with head 11
Main circuit, the main control component of aircraft 100, and head 11 can as unmanned vehicle 100 profile frame and main branch
Support body, head 11 is also used as the decorative element of unmanned vehicle 100.In order to lift the air force of unmanned vehicle 100
Performance, unmanned vehicle 100 can be designed to streamlined moulding.
The rear end of head 11 is provided with frame 12, and battery modules 3 and medicine-chest module 4 are arranged in frame 12.Wherein frame
12 structure can be arbitrary, as long as it can install battery modules 3 and medicine-chest module 4.As Figure 1-Figure 4, exist
In embodiments of the invention, the agent structure of frame 12 can be by being arranged on the rear end of head 11 and symmetrical relative to left and right directions
The installing plate of two strips set is constituted.Battery modules 3 and medicine-chest module 4 are clamped between two installing plates.
Wherein, battery modules 3 are as power source, for providing the power of whole unmanned vehicle 100, battery modules 3
It is detachably arranged in frame 12.Wherein it is understood that unmanned vehicle 100 according to embodiments of the present invention enters battery
Row modularization is set, and is demountable structure relative to frame 12, so that in terms of existing technologies, battery modules 3
Installation and removal are easier, so as to improve the assembling speed of unmanned vehicle 100 to a certain extent, when shortening assembling
Between.
Medicine-chest module 4 is used to store decoction, and wherein medicine-chest module 4 is detachably arranged in frame 12.In other words, medicine-chest mould
Group 4 has also carried out modular design as the memory unit of decoction, and is demountable structure relative to frame 12, so when
When needing to carry out supplement decoction to medicine-chest module 4, medicine-chest module 4 can directly be disassembled from frame 12 and be filled
Dress, it is filling finish after attach it to again in frame 12, mount and dismount it is fast and convenient, so as to can further improve nothing
The assembling speed of people's aircraft 100, improves service efficiency.
In an embodiment of the present invention, medicine-chest module 4 be located between head 11 and battery modules 3, specifically, Fig. 1-
In example shown in Fig. 4, head 11 is located at the front end of fuselage 1, and battery modules 3 are arranged on the rear portion of fuselage 1, and medicine-chest module 4 is front and rear
It is arranged on direction between head 11 and battery modules 3.
It is to be appreciated that with the flight course of unmanned vehicle 100, the sprinkling of decoction is constantly carried out, thus medicine-chest
Decoction in module 4 can be gradually decreased, and the weight of medicine-chest module 4 can be gradually reduced.And in the unmanned flight of the embodiment of the present invention
In device 100, medicine-chest module 4 is arranged between head 11 and battery modules 3, so that medicine-chest module 4 is located in the structure of fuselage 1
Portion, even if the weight of medicine-chest module 4 gradually changes also will not produce excessive influence, nothing to the overall center of gravity of unmanned vehicle 100
The position of centre of gravity of people's aircraft 100 is relatively stablized, and then the flight of unmanned vehicle 100 is more steady.
Alternatively, the decoction in medicine-chest module 4 can be sprayed by shower nozzle module 5, shower nozzle module 5 and medicine-chest module
4 are connected, wherein " shower nozzle module 5 is connected with medicine-chest module 4 " described here referring to that shower nozzle module 5 can be straight with medicine-chest module 4
Connect and be connected or be indirectly connected to.The opening for liquid communication can be for example provided with shower nozzle module 5, can be with medicine-chest module 4
Provided with the opening for liquid communication, two openings are joined directly together, so as to so that the liquid storage in medicine-chest module 4 flows to Nozzle At The Ingot Mold
Group 5 is sprayed；Or connecting conduit can be provided between medicine-chest module 4 and shower nozzle module 5, so as to by medicine-chest module 4
Interior liquid storage guide spray head module 5 is sprayed.As long as between shower nozzle module 5 and medicine-chest module 4 fluid connection can be carried out i.e.
Can.
Wherein, shower nozzle module 5 is provided with spout, and shower nozzle module 5 can be rotated during sprinkling, by decoction equably
Sprayed.Wherein shower nozzle module 5 can be driven rotation by motor.
Pump housing module is used to the decoction in medicine-chest module being pumped into Nozzle At The Ingot Mold group, and pump housing module is located on fuselage and is located at
Below head.Electric mode transfer group is used for automatically controlled regulation, and electric mode transfer group is located on fuselage and below head, and electric mode transfer group is used to control
It can be entered the operation of motor processed, the motor 30, the motor of shower nozzle module 5 such as driving rotor 20 by electric mode transfer group
Row control.
In one embodiment of the invention, alternatively, as shown in figure 4, limiting section 32 can be provided with battery modules 3,
Limiting section 32 is used to be pressed on medicine-chest module 4, to limit the free degree that medicine-chest module 4 is moved upwards.Due to battery modules 3
With certain weight, medicine-chest module 4 can so be suppressed using the weight of battery modules 3, it is to avoid lower thereon to occur
Vibrate and influence to use, improve the mounting stability of medicine-chest module 4.
Unmanned vehicle 100 according to embodiments of the present invention, by the way that battery modules 3 and medicine-chest module 4 are carried out into modularization
Design and be removably connected between frame 12, so as to so that the installation and removal of battery modules 3 and medicine-chest module 4 more
It is easy to be quick, the packaging efficiency of unmanned vehicle 100 is improved, operating efficiency is improved.In addition, by the way that medicine-chest module 4 is set
Put between head 11 and battery modules 3, so that when medicine-chest module 4 is as the liquid level of decoction changes and occurs mass change
When, because medicine-chest module 4 is in the middle part of fuselage 1, so that the position of centre of gravity of unmanned vehicle 100 is relatively stablized, it is ensured that nobody
The having a smooth flight property of aircraft 100.It is used to be pressed on the jacket of medicine-chest module 4 limitation medicine-chest further, since battery modules 3 are provided with
The free degree limiting section 32 that module 4 is moved upwards, from the mounting stability of medicine-chest module 4 can be improved.
Unmanned vehicle 100 according to embodiments of the present invention is described in detail below with reference to Fig. 1-Fig. 4.
In example as shown in Figure 1, battery modules 3 include multiple batteries (not shown) and battery case 31, multiple
Battery is integrated in battery case 31, can carry out series, parallel between multiple batteries as needed or series-parallel connection is set,
The inside of battery case 31 is provided with the detent mechanism for being used for installing locating batteries core, to ensure battery inside battery case 31
Mounting stability.Wherein, battery case 31 is slidably disposed in frame 12 in the vertical direction, that is to say, that battery case
31 can be inserted or pulled out frame 12 with the vertical direction, it is possible thereby to make the easier for installation of battery modules 3, facilitate battery
Replacing.
Alternatively, in an embodiment of the present invention, one in battery case 31 and frame 12 is provided with chute and another
It is individual provided with the slide rail slidably coordinated with chute, such as be provided with battery case 31 in chute, frame 12 and slide rail be set；Or
It is provided with person's frame 12 on chute, battery case 31 and slide rail is set.Cooperation by slide rail and chute can be battery case
Guiding positioning action is played in 31 inserting.In order to ensure the installation and removal on the above-below direction of battery case 31, slide rail and chute
Bearing of trend be above-below direction, thus after battery case 31 is installed in place, the fit structure of slide rail and chute can be with
Positioning action is played to the position of battery case 31 in the longitudinal direction, and then battery case 31 can be limited in the longitudinal direction
The free degree.
In order to improve the stable connection between battery case 31 and frame 12, battery case 31 and frame 12 can be connected with clamping
Connect.Specifically, can be set on battery case 31 in buckle, frame 12 can set neck, when battery case 31 is to underthrust
When entering onto frame 12, buckle just coordinates neck, so as to play fixation, or battery to battery case 31
Being also provided with shell 31 in the lock with latch functions, frame 12 can be provided with hole be fixedly mounted, and lock is with fixing peace
Dress hole coordinates and can also play fixation to battery case 31, and the present invention is not limited thereto certainly, when battery case 31 is installed
After on to frame 12, battery case 31 can also be fixed by single parts, for example threaded connector is locked
Only, the mode such as hawser binding is fixed.
In some preferred exemplaries, the electrical connector that mutual cooperation is respectively equipped with frame 12 and battery case 31 (is schemed not
Show), electrical connector after battery modules 3 are installed in place on battery case 31 is docked with the electrical connector in frame 12.Tool
Body, the electricity consumption device that the electrical connector in frame 12 can be with unmanned vehicle 100 by way of cable is connected is connected
Connect, such as the motor 30 for driving rotor 20, the motor of shower nozzle module 5, so when battery case 31 is installed in place
Afterwards, it can be electrically connected by the electrical connector in frame 12 with electricity consumption device, it is possible thereby to simplify battery modules 3 and electricity consumption device
Between electric connection structure, it is convenient to install.Advantageously, the electrical connector on the electrical connector and frame 12 on battery case 31 can
To carry out arrangement arrangement in the vertical direction, it is possible thereby to be made using the self gravitation of battery modules 3 suitable between two electrical connectors
Sharp grafting in place, prevents void from inserting situation.
Certainly the present invention is not limited thereto, after battery modules 3 are installed in place, can also pass through connection cables with it is corresponding
Electricity consumption device is attached.
In an embodiment of the present invention, alternatively, medicine-chest module 4 is slidably disposed in frame 12 in the vertical direction.
Alternatively, medicine-chest module 4 can also be coordinated with frame 12 by chute rail structure, thus both can be to medicine-chest module 4
Installation play guide function, can be also used for limitation medicine-chest module 4 free end in the longitudinal direction, it is ensured that install stable
Property.
Further, as shown in figure 1, frame 12 is provided with brace rod 121, medicine-chest module 4 is provided with multiple opening down
Neck, multiple necks are respectively supported on brace rod 121, that is to say, that can be limited by the cooperation of neck and brace rod 121
The free degree that pharmacy case module 4 is moved downward.Wherein alternatively, brace rod 121 can be made up of the top edge of frame 12.
Specifically, shown in Figure 1, medicine-chest module 4 includes casing 41 and the case lid 42 being located on casing 41, and decoction is filling
In casing 41, case lid 42 can open or close casing 41.Alternatively, in the relative two side wall of case lid 42 each is equal
Provided with multiple lug bosses 421, neck formation is on the lower surface of lug boss 421.In other words, the left surface and right flank of case lid 42
On be respectively equipped with lug boss 421, left surface is provided with can be provided with one or more lug bosses 421, right flank and can also set
There are one or more lug bosses 421, the lower end of each lug boss 421 is each formed with neck, it is possible thereby to make medicine-chest module 4 in machine
Installation on frame 12 is more stablized.
In order to extract conveniently, handle 423 is additionally provided with case lid 42.Alternatively, the hardness of case lid 42 is more than the hard of casing 41
Degree, it is possible thereby on the premise of the stability that case lid 42 is fixed with frame 12 is improved, reduce the weight of medicine-chest module 4.
Alternatively, as shown in figure 1, the filling exit for liquid drug can be provided with case lid 42, that is to say, that decoction is not
It can be only directly injected into casing 41, after can also the filling exit on case lid 42 be opened, passed through after case lid 42 by opening
Filling exit carries out the filling of decoction.Spiral cover 422 can be provided with filling exit, spiral cover 422 can cover the filling exit, so as to avoid
Decoction is spilt.Preferably, the spiral cover 422 can be passed through with supplied gas, to avoid during medicine liquid spray, medicine-chest module 4 and extraneous ring
Effect between border due to pressure differential causes liquid to have some setbacks.
When to battery modules 3 and the installation of medicine-chest module 4, because the position limiting structure of the limiting sections 32 of battery modules 3 is deposited
, therefore first medicine-chest module 4 should be inserted into frame 12 from top to bottom, then battery modules 3 are inserted into machine from top to bottom
On frame 12, and medicine-chest module 4 is pressed against using position limiting structure.Of course, it should be understood that dismounting process be it is opposite, it is necessary to
Now battery modules 3 are proposed upwards from frame 12, then medicine-chest module 4 is dismantled.Such installation and removal process, can
To play foolproof function, i.e., after first battery modules 3 are disassembled, then medicine-chest module 4 is dismantled, so as to prevent artificial behaviour by mistake
Make, when no dismounting battery modules 3, when just medicine-chest module 4 is first dismantled, decoction drop is splashed in battery modules 3 and produced
Raw circuit safety problem.
Unmanned vehicle 100 according to embodiments of the present invention, alternatively, shower nozzle module 5 is detachably arranged on horn 2.
For example shower nozzle module 5 can be located at by threaded fastener on corresponding horn 2, specifically, and shower nozzle module 5 includes shell
51st, motor and spray disk 52, spray disk 52 are arranged on the motor shaft of motor, and motor is located in shell 51, shell
51 can be located at by threaded fastener on corresponding horn 2, it is possible thereby to make attachment structure between shower nozzle module 5 and horn 2
Simply, and the purpose of fast assembling-disassembling can be realized.Certainly the present invention is not limited thereto, and shower nozzle module 5 can also pass through buckle
On the corresponding horn 2 of structure setting.
Alternatively, shower nozzle module 5 can be configured to use the structure that centrifugal force is sprayed.That is, spray disk 52
It can be rotatable structure, during spray 52 high-speed rotation of disk, decoction can be made to be sprayed under the influence of centrifugal force.
Using centrifugal sprinkler module 5 to decoction carry out centrifugal atomizing so that medicine liquid spray evenly, so as to carry
The utilization rate of high decoction, and the descending air-flow when rotor 20 of unmanned vehicle rotates is combined more effectively by the medicine of centrifugal atomizing
Liquid spray attachment drug effect fruit more preferable below crop leaf.
Wherein in an embodiment of the present invention, horn 2 is multiple, and multiple horns 2 are provided at circumferentially spaced around fuselage 1.Spray
Head mould group 5 is located at least a portion of multiple horns 2, that is to say, that shower nozzle module 5 can be arranged on one in multiple horns 2
Shower nozzle module 5 is respectively provided with part, or on each horn 2.Alternatively, in one embodiment of the invention, shower nozzle module 5
Quantity it is identical with the quantity of horn 2, and multiple shower nozzle modules 5 are detachably arranged in the bottom of the end of multiple horns 2 respectively.
Specifically, shower nozzle module 5 is arranged on the bottom of the end of horn 2.Thus multiple dispersed placements of shower nozzle module 5, therefore meet liquid medicine jet
Requirement is spilt, hydrojet is more uniform.
Correspondingly, in example as Figure 1-Figure 4, the end of each horn 2 is equipped with rotor 20 and driving rotor 20
The motor 30 of rotation, rotor 20 can be connected with the motor shaft of motor 30, and motor 30 is electrically connected with battery modules 3, to make rotation
The rotation of the wing 20 is so as to drive unmanned vehicle 100 to be flown.Shower nozzle module 5 can be arranged on the underface of motor 30.Wherein
Shower nozzle module 5 can be rotated to be sprayed decoction, therefore alternatively, shower nozzle module 5 can be driven by motor 30
Dynamic rotation, or shower nozzle module 5 can be driven with separately installed motor.
Alternatively, it can be connected between medicine-chest module 4 and shower nozzle module 5 by infusion channel (not shown), horn 2
End relevant position can set the opening connected with infusion channel, can be with this when shower nozzle module 5 is installed on horn 2
Be open corresponding matching, so as to be connected with infusion channel, and then is connected with medicine-chest module 4, so as to carry out sprinkling decoction.
In such as example shown in Fig. 1 and Fig. 3, horn 2 include four, four horns 2 be respectively provided at the front left side of fuselage 1,
Forward right side, left rear side and right lateral side, four horns 2 can be in X-shaped distribution.Shower nozzle module 5 includes four and set respectively accordingly
On four horns 2.
Wherein it should be noted that alternatively, horn 2 can be connected to the bottom of head 11, the horn 2 of front left side, it is right before
The horn 2 of side is symmetrical, and the horn 2 of left rear side, the horn 2 of right lateral side are symmetrical, the extended line of four horns 2
Approximate intersection point can be located on the forward position in the middle part of head 11, it is possible thereby to make medicine-chest module 4 and battery modules 3 in fuselage 1
The arrangement at middle part and rear portion can be slightly forward, makes the center in fuselage 1 of the center of gravity of unmanned vehicle 100 approximately,
As the decoction in medicine-chest module 4 is gradually decreased in the operation process of unmanned vehicle 100, because it is in center, nobody flies
Too big skew will not occur for the center of gravity of row device 100, further ensure the flight of unmanned vehicle 100.
In an embodiment of the present invention, pump housing module is removably set on the fuselage 1 and neighbouring medicine-chest module 4 is set
Put.That is, the unmanned vehicle 100 of the present invention, by removably connecting by pump body structure modularity, and with fuselage 1
Connect, so as to improve the installation effectiveness of pump housing module, mount and dismount easier.Specifically, alternatively, the present invention is real
Apply in example, pump housing module can include multiple liquid pumps and pump housing shell, plurality of liquid pump (not shown) is located at pump housing shell
Interior, pump housing shell is detachably arranged on fuselage 1.Alternatively, pump housing module may be mounted at the bottom of the head 11 of fuselage 1,
It is possible thereby to increase the weight of the part of head 11, the center of gravity for adjusting whole unmanned vehicle 100.
Specifically, multiple liquid pumps are connected with multiple shower nozzle modules 5 by infusion channel respectively, that is to say, that pump housing module is used
Decoction in by medicine-chest module 4 is delivered in corresponding shower nozzle module 5, is corresponded, it is possible thereby to make each shower nozzle module 5
Hydrojet can individually control, it is easy to use, and can make it that complete machine stringing is clean and tidy, is easy to check and changes maintenance.
Preferably, in an embodiment of the present invention, at least one in multiple liquid pumps is peristaltic pump.Thus on the one hand can be with
Decoction is avoided to be corroded peristaltic pump with peristaltic pump interior contact, or decoction is polluted；Another aspect peristaltic pump with
Other kinds of pump is compared, and has the advantages that small volume, lightweight, energy consumption are low, it is possible thereby to be more suitable for unmanned vehicle
Miniaturization Design.
Alternatively, electric mode transfer group can removably be located at the bottom of fuselage 1.Thus, electric mode transfer group can be square
Just installation and removal.Wherein electric mode transfer group can be arranged on the bottom of head 11, it is possible thereby to increase the weight of the part of head 11
Amount, the center of gravity for adjusting whole unmanned vehicle 100.In addition, electric mode transfer group includes circuit board assemblies and metal framework, circuit
Board component is located inside metal framework, and metal framework is located at the bottom of head 11, so as to utilize the metal framework to head
11 structure plays a part of reinforcing.Specifically, the bottom of head 11 has head plate body and is located on head plate body
Head encloser, the metal framework of electric mode transfer group is located on the lower surface of the head plate body, so that metal framework can be to machine head plate
The structure of body plays a part of reinforcement.Electric mode transfer group is located at the front portion of pump housing module.
As shown in figure 4, unmanned vehicle 100 also includes drain pan 40, drain pan 40 is located at outside pump housing module and electric mode transfer group
Portion, it is possible thereby to playing a part of the sandy soil dust in protection, barrier operating environment outside pump housing module and electric mode transfer group, keep away
Exempt from the electric control part of the electric mode transfer group of decoction drift bespatter dye.Preferably, openwork part can be provided with the drain pan 40, electricity is thereby guaranteed that
The radiating effect of mode transfer group.
Below with reference to Fig. 1 and Fig. 2, as illustrated, the unmanned vehicle 100 of the embodiment of the present invention also include being used to receive and
Send the difference module 7 (such as RTK antennas, Real-time kinematic real time dynamic differentials antenna) of signal, difference module
7 are located on horn 2, and such mounting structure makes that the fixation of difference module 7 is reasonable, mounting structure is succinct.
As shown in figure 1, being provided with two difference modules 7, the straight line of the two difference modules 7 on unmanned vehicle 100
Spacing distance needs to be maintained at more than 45cm, in the prior art, is strutted between two difference modules by support bar, or will
Two difference modules are fixed in the other structures of aircraft.It will be strutted, then can increased with support bar between two difference modules
Main screw lift, total is not succinct enough, and causes cost to increase；And by two difference modules be fixed on aircraft other
In structure, then probably due to housing construction insufficient space, RTK antenna measurement precision is impacted, or even it can be interfered.It is based on
This, in the embodiment of the present invention, two difference modules 7 is separately positioned on the horn 2 of the right lateral side of fuselage 1 and the horn 2 of left rear side
On, so it can ensure to be arranged on two horns using the chi structure between the horn 2 of right lateral side and the horn 2 of left rear side
Naturally the requirement of above-mentioned straight line spacing is met between difference module 7 on 2, it is possible thereby to will not only increase extra installation
Structure, reduces cost, and ensure that the rational in infrastructure succinct of unmanned vehicle 100, complete appearance.
Alternatively, mounting structure of the difference module 7 on horn 2 can be arbitrary, for example, can lead to difference module 7
Cross buckle structure to be directly installed on horn 2, specifically, neck can be provided with horn 2, offers on difference module 7 and sets
There is buckle, buckle and neck coordinate difference module 7 being directly anchored on horn 2；Or difference module 7 can also pass through spiral shell
Line structure is directly installed on horn 2, specifically, and can be provided with external screw thread, horn 2 on the perisporium of difference module 7 to be provided with
Have female groove, pass through engaging so that difference module 7 is directly installed on horn 2 for external screw thread and internal thread.
In addition, difference module 7 can also be indirectly mounted on horn 2 by other structures.In the tool of the present invention
In body example, difference module 7 is located on horn 2 by dismountable mode, it is possible thereby to facilitate the peace installation and dismantling of difference module 7
Unload.Specifically, as shown in Fig. 2 unmanned vehicle 100 also includes mounting bracket 8, wherein difference module 7 is located at mounting bracket 8
On, mounting bracket 8 is detachably arranged on horn 2 by yoke configurations 81.Installed indirectly from there through using mounting bracket 8
On horn 2, so as to play reinforcement effect to difference module 7, the installation of difference module 7 is more stablized, and can prevent difference
Point module 7 after external impacts by causing to damage.
Further, structure can be connected through a screw thread between difference module 7 and mounting bracket 8 to be connected, it is possible thereby to right
Difference module 7 carries out Fast Installation and replacement.
As Figure 1-Figure 4, the unmanned vehicle 100 of the embodiment of the present invention also includes foot stool 10, and foot stool 10 is removably
The bottom of head 11 is located at, foot stool 10 includes at least one foot stool 10, and wherein foot stool 10 is the lath being made up of carbon fibre material
Part.Firstly, since foot stool 10 is set into slat element structure, so as to increase the contact area of foot stool 10 and ground, improve
The stability of landing.Secondly as carbon fibre material has excellent resilience characteristic, during unmanned vehicle 100 lands,
Cushioning effect can be played to unmanned vehicle 100 by possessing certain elasticity, so as to protect other modules of unmanned vehicle 100
It is not easily damaged.Wherein, foot stool 10 can be integrally formed, it is possible thereby to be easy to assembling to produce.And it is lightweight,
Wherein, foot stool 10 is can be seen that using substantially trapezium structure from Fig. 4 side view, so in unmanned vehicle 100
Front and rear load-bearing position can play a supporting role.As can be seen that foot stool 10 is two and two foot stools 10 from Fig. 1 stereogram
Arrange and install in "eight" shape in the lateral direction, thereby guarantee that unmanned vehicle 100 is difficult rollover after landing.
In summary, according to the description of the unmanned vehicle 100 of the above-mentioned some embodiments of the present invention, according to present invention implementation
The unmanned vehicle 100 of example can have following improvement and corresponding beneficial effect：
1st, by the way that battery modules 3 and medicine-chest module 4 are carried out into modularized design and are removably connected between frame 12,
So as to improve the packaging efficiency of unmanned vehicle 100；
2nd, by the way that medicine-chest module 4 is arranged between head 11 and battery modules 3, so that the center of gravity of unmanned vehicle 100
Relatively stablize position, it is ensured that the having a smooth flight property of unmanned vehicle 100；
3rd, can be with by by equal modularized designs of structure such as shower nozzle module 5, pump housing module, electric mode transfer group, difference modules 7
It is easy to the dismounting and maintenance of each module；
4th, medicine-chest module 4 and battery modules 3 have priority loading order, so as to play foolproof function, it is to avoid decoction
Drop is splashed in battery modules 3 and generation circuit safety problem；
5th, foot stool 10 is the slat element that is made up of carbon fibre material, so as to increase the contact area with ground, and
Cushioning effect is played in descent to unmanned vehicle 100, integrally formed slat element easily facilitates assembling production；
6th, difference module 7 is arranged on the horn 2 of the right lateral side of fuselage 1 and the horn 2 of left rear side, both ensure that unmanned vehicle
100 outward appearance globality, and the rotation of rotor 20 is not influenceed.
In the description of this specification, reference term " one embodiment ", " some embodiments ", " illustrative examples ",
The description of " example ", " specific example " or " some examples " etc. means to combine specific features, the knot that the embodiment or example are described
Structure, material or feature are contained at least one embodiment of the present invention or example.In this manual, to above-mentioned term
Schematic representation is not necessarily referring to identical embodiment or example.Moreover, specific features, structure, material or the spy of description
Point can in an appropriate manner be combined in any one or more embodiments or example.
Although an embodiment of the present invention has been shown and described, it will be understood by those skilled in the art that：Not
In the case of departing from the principle and objective of the present invention a variety of change, modification, replacement and modification can be carried out to these embodiments, this
The scope of invention is limited by claim and its equivalent.
Claims (16)
1. a kind of unmanned vehicle, it is characterised in that including：
Fuselage, the fuselage has head, and the rear end of the head is provided with frame；
Multiple horns, the multiple horn is provided at circumferentially spaced around the fuselage；
Battery modules for providing power, the battery modules are detachably arranged in the frame；
Medicine-chest module for storing decoction, the medicine-chest module is detachably arranged in the frame and medicine-chest module position
Between the head and the battery modules, the medicine-chest module and the battery modules are distributed along the longitudinal direction, wherein institute
Battery modules are stated provided with limiting section, the limiting section support is pressed on the medicine-chest module transports upwards to limit the medicine-chest module
The dynamic free degree；
Shower nozzle module for spraying decoction, the shower nozzle module be located at least a portion of the multiple horn and with it is described
Medicine-chest module is connected；
For the pump housing module being pumped into the decoction in the medicine-chest module in the shower nozzle module, the pump housing module is located at institute
State on fuselage and below the head；
For the electric mode transfer group of automatically controlled regulation, the electric mode transfer group is located on the fuselage and below the head.
2. unmanned vehicle according to claim 1, it is characterised in that the battery modules include multiple batteries and electricity
Pond shell, the multiple battery is integrated in the battery case, and the battery case is slideably set in the vertical direction
In the frame.
3. unmanned vehicle according to claim 2, it is characterised in that one in the battery case and the frame
It is provided with chute and another is provided with the slide rail slidably coordinated with the chute.
4. the unmanned vehicle according to any one of Claims 2 or 3, it is characterised in that the frame and the battery
The electrical connector of mutual cooperation is respectively equipped with shell, being electrically connected on the battery case after battery modules are installed in place
Fitting is docked with the electrical connector in the frame.
5. unmanned vehicle according to claim 1, it is characterised in that the medicine-chest module is in the vertical direction slidably
Ground is located in the frame.
6. unmanned vehicle according to claim 5, it is characterised in that the frame is provided with brace rod, the medicine-chest
Module is provided with multiple downward opening necks, and the multiple neck is respectively supported on the brace rod.
7. unmanned vehicle according to claim 6, it is characterised in that the medicine-chest module includes casing and is located at described
Each in case lid on casing, the relative two side wall of the case lid is equipped with multiple lug bosses, and the neck is formed
On the lower surface of the lug boss.
8. unmanned vehicle according to claim 1, it is characterised in that the shower nozzle module includes multiple, and the pump
Body module includes multiple liquid pumps and pump housing shell, and the multiple liquid pump passes through infusion channel phase with the multiple shower nozzle module respectively
Connect and the multiple liquid pump is located in the pump housing shell, the pump housing shell is detachably arranged on the fuselage.
9. unmanned vehicle according to claim 8, it is characterised in that the quantity of the shower nozzle module and the horn
Quantity is identical, and the multiple shower nozzle module is detachably arranged in the bottom of the end of the multiple horn respectively.
10. unmanned vehicle according to claim 8, it is characterised in that at least one in the multiple liquid pump
For peristaltic pump.
11. unmanned vehicle according to claim 1, it is characterised in that also including the difference for receiving and sending signal
Divide module, the difference module is located on the horn.
12. unmanned vehicle according to claim 11, it is characterised in that also including mounting bracket, the difference module
It is located in the mounting bracket, the mounting bracket is detachably arranged on the horn by yoke configurations.
13. unmanned vehicle according to claim 1, it is characterised in that the shower nozzle module is by being detachably arranged in
On the corresponding horn.
14. unmanned vehicle according to claim 1, it is characterised in that also including foot stool module, the foot stool module can
The bottom of the head is releasably located at, the foot stool module includes at least one foot stool, wherein the foot stool is by carbon fiber
The slat element that material is made.
15. unmanned vehicle according to claim 1, it is characterised in that also including drain pan, the drain pan is located at described
Outside pump housing module and the electric mode transfer group.
16. unmanned vehicle according to claim 1, it is characterised in that the shower nozzle module is configured to use centrifugation
The structure that power is sprayed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610214440.6A CN105752340B (en) | 2016-04-07 | 2016-04-07 | Unmanned vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610214440.6A CN105752340B (en) | 2016-04-07 | 2016-04-07 | Unmanned vehicle |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105752340A CN105752340A (en) | 2016-07-13 |
| CN105752340B true CN105752340B (en) | 2017-09-01 |
Family
ID=56333562
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610214440.6A Active CN105752340B (en) | 2016-04-07 | 2016-04-07 | Unmanned vehicle |
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| CN (1) | CN105752340B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11811224B2 (en) | 2017-04-07 | 2023-11-07 | Mark Holbrook Hanna | Distributed-battery aerial vehicle and a powering method therefor |
Families Citing this family (21)
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|---|---|---|---|---|
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| CN206218204U (en) * | 2016-11-18 | 2017-06-06 | 深圳市大疆创新科技有限公司 | Aircraft |
| CN106892116A (en) * | 2017-02-27 | 2017-06-27 | 四川雷神空天科技有限公司 | For the flight instruments platform and its system and operational method of plant protection operation |
| CN107187586B (en) * | 2017-04-28 | 2023-09-15 | 北京远度互联科技有限公司 | Unmanned vehicles organism and unmanned vehicles |
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| CN107878755A (en) * | 2017-10-24 | 2018-04-06 | 江苏精微特电子股份有限公司 | A kind of agricultural spray unmanned plane |
| CN108100214A (en) * | 2018-01-05 | 2018-06-01 | 河南正大航空科技股份有限公司 | A kind of spray formula unmanned plane frame structure |
| WO2020113445A1 (en) * | 2018-12-04 | 2020-06-11 | 深圳市大疆创新科技有限公司 | Agricultural unmanned aerial vehicle |
| CN109455291A (en) * | 2018-12-25 | 2019-03-12 | 拓攻（南京）机器人有限公司 | A kind of rack and unmanned plane for unmanned plane |
| CN109733610A (en) * | 2019-01-28 | 2019-05-10 | 河南正大航空工业股份有限公司 | A kind of novel modularized unmanned plane |
| CN109720559A (en) * | 2019-02-25 | 2019-05-07 | 深圳市翔农创新科技有限公司 | A kind of plant protection drone of novel layouts |
| CN111216868A (en) * | 2019-08-27 | 2020-06-02 | 苏州极目机器人科技有限公司 | Frame for aircraft and aircraft |
| CN111409827B (en) * | 2020-04-08 | 2023-07-18 | 贵州电网有限责任公司 | Use convenient hoist mechanism and unmanned aerial vehicle |
| WO2022120810A1 (en) * | 2020-12-11 | 2022-06-16 | 深圳市大疆创新科技有限公司 | Multi-rotor plant protection unmanned aerial vehicle |
| WO2023184117A1 (en) * | 2022-03-28 | 2023-10-05 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle, antenna assembly, and antenna support |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN203612209U (en) * | 2013-11-26 | 2014-05-28 | 山东新晨科技有限公司 | Agricultural aircraft |
| JP5809422B2 (en) * | 2011-02-25 | 2015-11-10 | ニューデルタ工業株式会社 | Unmanned helicopter |
| CN105059547A (en) * | 2015-08-17 | 2015-11-18 | 山东卫士植保机械有限公司 | Multi-rotor unmanned pesticide application machine |
| CN105253304A (en) * | 2015-11-03 | 2016-01-20 | 南京林业大学 | Multi-rotor unmanned aerial vehicle variable spraying system |
-
2016
- 2016-04-07 CN CN201610214440.6A patent/CN105752340B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP5809422B2 (en) * | 2011-02-25 | 2015-11-10 | ニューデルタ工業株式会社 | Unmanned helicopter |
| CN203612209U (en) * | 2013-11-26 | 2014-05-28 | 山东新晨科技有限公司 | Agricultural aircraft |
| CN105059547A (en) * | 2015-08-17 | 2015-11-18 | 山东卫士植保机械有限公司 | Multi-rotor unmanned pesticide application machine |
| CN105253304A (en) * | 2015-11-03 | 2016-01-20 | 南京林业大学 | Multi-rotor unmanned aerial vehicle variable spraying system |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11811224B2 (en) | 2017-04-07 | 2023-11-07 | Mark Holbrook Hanna | Distributed-battery aerial vehicle and a powering method therefor |
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