CN108271759A - A kind of multi-rotor unmanned aerial vehicle sprinkling system - Google Patents

A kind of multi-rotor unmanned aerial vehicle sprinkling system Download PDF

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Publication number
CN108271759A
CN108271759A CN201810230280.3A CN201810230280A CN108271759A CN 108271759 A CN108271759 A CN 108271759A CN 201810230280 A CN201810230280 A CN 201810230280A CN 108271759 A CN108271759 A CN 108271759A
Authority
CN
China
Prior art keywords
aerial vehicle
shunting
unmanned aerial
sprinkling system
rotor unmanned
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201810230280.3A
Other languages
Chinese (zh)
Inventor
杨凌
文朋
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Chaonongli (Zhejiang) Intelligent Technology Co.,Ltd.
Original Assignee
Chengdu Tianqi Technology Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Chengdu Tianqi Technology Co Ltd filed Critical Chengdu Tianqi Technology Co Ltd
Priority to CN201810230280.3A priority Critical patent/CN108271759A/en
Publication of CN108271759A publication Critical patent/CN108271759A/en
Pending legal-status Critical Current

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Classifications

    • AHUMAN NECESSITIES
    • A01AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
    • A01MCATCHING, TRAPPING OR SCARING OF ANIMALS; APPARATUS FOR THE DESTRUCTION OF NOXIOUS ANIMALS OR NOXIOUS PLANTS
    • A01M7/00Special adaptations or arrangements of liquid-spraying apparatus for purposes covered by this subclass
    • A01M7/0025Mechanical sprayers
    • A01M7/0032Pressure sprayers
    • AHUMAN NECESSITIES
    • A01AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
    • A01MCATCHING, TRAPPING OR SCARING OF ANIMALS; APPARATUS FOR THE DESTRUCTION OF NOXIOUS ANIMALS OR NOXIOUS PLANTS
    • A01M7/00Special adaptations or arrangements of liquid-spraying apparatus for purposes covered by this subclass
    • A01M7/005Special arrangements or adaptations of the spraying or distributing parts, e.g. adaptations or mounting of the spray booms, mounting of the nozzles, protection shields
    • AHUMAN NECESSITIES
    • A01AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
    • A01MCATCHING, TRAPPING OR SCARING OF ANIMALS; APPARATUS FOR THE DESTRUCTION OF NOXIOUS ANIMALS OR NOXIOUS PLANTS
    • A01M7/00Special adaptations or arrangements of liquid-spraying apparatus for purposes covered by this subclass
    • A01M7/0089Regulating or controlling systems
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D1/00Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
    • B64D1/16Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting
    • B64D1/18Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting by spraying, e.g. insecticides
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV
    • B64U10/10Rotorcrafts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00UAVs specially adapted for particular uses or applications

Abstract

The present invention discloses a kind of multi-rotor unmanned aerial vehicle sprinkling system, including:Medicine-chest is arranged on unmanned plane body, for storing liquid;Dispenser, there are one inlets and two liquid outlets, the inlet to be connected to medicine-chest inner cavity for the dispenser tool;The pump housing, including pump intake and pump discharge, the pump intake is connected to liquid outlet, for driving liquid medicine flow;Guider is shunted, there are one shunting import and two shunting outlets, shunting imports to be connected to pump intake for the shunting guider tool, shunts and is provided with solenoid valve on guider, and the solenoid valve is for controlling shunting outlet break-make;The present invention is intended to provide a kind of multi-rotor unmanned aerial vehicle sprinkling system, it can be in unmanned plane job run, water pump does not stop, by controlling the control valve inside shunting guider, water route switching is carried out, to mitigate unmanned plane body weight, to improve the flight time, increase battery durable ability, increases operating efficiency.

Description

A kind of multi-rotor unmanned aerial vehicle sprinkling system
Technical field
The present invention relates to air vehicle technique field more particularly to a kind of multi-rotor unmanned aerial vehicle sprinkling systems.
Background technology
Currently, as land transformation, farm land produce gradual scale, to improve agricultural production efficiency, reducing agricultural Production cost, the demand that operations such as spraying insecticide are carried out using unmanned plane are increased increasingly.The four nozzle plant protection of existing more rotors without It is man-machine, it mostly uses " one-to-one " peristaltic pump and centrifugal energy nozzle or the diaphragm pump of " a pair two " is added to add high pressure the spray pattern of nozzle, plant It protects in flight course, there are the states that one or more water pump leaves unused always.To improve unmanned plane operating efficiency and efficiency, need Sprinkling system structure is reduced as far as possible, and then mitigates unmanned plane body weight, to improve the flight time, increases battery durable Ability increases operating efficiency.
Invention content
The present invention is intended to provide a kind of multi-rotor unmanned aerial vehicle sprinkling system, it can be in unmanned plane job run, water pump is not Stop, by controlling the control valve inside shunting guider, progress water route switching, to mitigate unmanned plane body weight, To improve the flight time, increase battery durable ability, increases operating efficiency.
In order to achieve the above objectives, the technical solution adopted by the present invention is as follows:
A kind of multi-rotor unmanned aerial vehicle sprinkling system, including:
Medicine-chest is arranged on unmanned plane body, for storing liquid;
Dispenser, there are one inlets and two liquid outlets, the inlet to be connected to medicine-chest inner cavity for the dispenser tool;
The pump housing, including pump intake and pump discharge, the pump intake is connected to liquid outlet, for driving liquid medicine flow;
Guider is shunted, there are one shunting imports and two to shunt outlet, shunting import and pump for the shunting guider tool Entrance is connected to, and is shunted and is provided with solenoid valve on guider, and the solenoid valve is for controlling shunting outlet break-make;
Centrifugal energy nozzle, in unmanned plane horn end, each centrifugal energy nozzle is described respectively with a shunting outlet for setting Centrifugal energy nozzle makes liquid carry out centrifugation sprinkling when rotating;The multiple centrifugal energy nozzle arranged for interval being connected to same liquid outlet are at nobody In machine circumferential direction.
In some embodiments, further include control module, the control module is for obtaining flight information and passing through flight Information controls the break-make of centrifugal energy nozzle start and stop and shunting outlet.
In some embodiments, the flight information includes course angle, the speed of a ship or plane and location information.
In some embodiments, the pump housing further includes installation shell, and the pump housing is fixed on unmanned plane machine by installing shell On body.
In some embodiments, the centrifugal energy nozzle includes:
Drainage disc, the drainage disc top are equipped with inlet tube, and drainage pan bottom is equipped with outlet tube;
Motor, the motor include body, shell and mounting disc, and the shell is fixed on above the drainage disc, shell Lower end is equipped with the protection axle sleeve extending into drainage disc;The shell and mounting disc limit the installation space of body, institute jointly Mounting disc is stated for centrifugal atomizing nozzle to be fixed on outer structural parts;The body include the movement that is arranged in shell and It is connected with the movement and across the protection axle sleeve to stretch out the arbor of drainage disc;
Atomization spray disk, atomization spray disk be located at drainage disc lower section and be provided with lead channel with accept from it is described go out liquid The liquid of pipe discharge, and connect with the arbor to drive atomization spray disc spins.
In some embodiments, the atomization spray disk includes:
Chassis, the lead channel are arranged in the middle part of chassis;
Multiple convex blocks, chassis upper surface and circumferentially-spaced uniformly distributed in chassis edge is arranged in the multiple convex block, per adjacent Two convex blocks between limit one centrifugation runner;
Multiple cylinders, the multiple cylinder are arranged between lead channel and convex block, and in multiple circumferential directions of chassis upper surface On uniformly at intervals to form multiple concentric circles band of columns, all cylinders limit centrifugal space jointly.
In some embodiments, the atomization spray disk further includes:
Multiple dividing strips, uniformly at intervals in the circumferential direction of chassis upper surface, dividing strip part is located at the multiple dividing strip It centrifuges in runner, dividing strip remainder is located in centrifugal space, for being carried out again to the fluid after centrifugal space is divided Segmentation.
In some embodiments, the two neighboring cylinder in external circumferential is smaller than positioned at inner circumferential On the two neighboring cylinder spacing.
In some embodiments, the chassis middle part is recessed so that upper surface forms the lead channel, and feed liquor groove center is solid Surely there is hollow cylinder, the hollow cylinder is for connecting arbor.
In some embodiments, the atomization spray disk further includes installing nut and lower end and being connected with the squash type of screw rod to fix Axle sleeve, squash type fixed hub top outer diameter are more than hollow cylinder outer diameter, and squash type fixed hub lower end passes through hollow cylinder simultaneously It is connect with installation nut, the arbor is inserted into squash type fixed hub and by installing nut and hollow cylinder to realize machine The fixation of axis and atomization spray disk.
Compared with prior art, the invention has the advantages that:
This invention simplifies the structures of unmanned plane sprinkling system, can be in unmanned plane job run, and water pump does not stop, and passes through Control valve inside shunting guider is controlled, water route switching is carried out, to mitigate unmanned plane body weight, to improve Flight time increases battery durable ability, increases operating efficiency.
Description of the drawings
Fig. 1 is schematic structural view of the invention;
Fig. 2 is sprinkling system structural schematic diagram;
Fig. 3 is sprinkling system functional block diagram;
Fig. 4 is line of flight schematic diagram;
Fig. 5 is centrifugal energy nozzle schematic diagram;
Fig. 6 is centrifugal energy nozzle explosive view;
Fig. 7 is atomization spray disk schematic diagram;
Fig. 8 is atomization spray disk explosive view;
Fig. 9 is chassis structure schematic diagram;
Figure 10 is chassis top view;
Figure 11 is enlarged drawing at A in Figure 10;
In figure:100- medicine-chests, 200- dispensers, the 300- pump housings, 400- shuntings guider, 500- centrifugal energy nozzles, 600- controls Molding block;
201- inlets, 202- liquid outlets;
301- pump intakes, 302- pump discharges;
401- shunts import, 402- shuntings outlet, 403- solenoid valves;
510- motors, 520- drainage discs, 530- atomization spray disks;
511- mounting discs, 512- bodies, 513- shells, 514- protections axle sleeve, 515- movements, 516- arbors;
The chassis 531-, 532- convex blocks, 533- cylinders, 534- dividing strips, 535- lead channel, 536- centrifugation runner, 537- from Heart space, 538- hollow cylinders;
541- installs nut, 542- squash types fixed hub, 543- screw rods, 544- external pressures part, the compression of the inside 545- Part.
Specific implementation mode
In order to make the purpose , technical scheme and advantage of the present invention be clearer, below in conjunction with attached drawing, to the present invention into Row is further described.
According to an embodiment of the invention, as shown in Figs. 1-3, a kind of multi-rotor unmanned aerial vehicle sprinkling system, including:Medicine-chest 100, Dispenser 200, the pump housing 300, shunting guider 400, centrifugal energy nozzle 500 and control module 600.
As shown in Figure 1, medicine-chest 100 is arranged on unmanned plane body, for storing liquid;Dispenser 200 tool there are one into Liquid mouth 201 and two liquid outlets 202, the inlet 201 are connected to 100 inner cavity of medicine-chest;The pump housing 300 includes 301 He of pump intake Pump discharge 302, pump intake 301 is connected to liquid outlet 202, for driving liquid medicine flow;Shunting the tool of guider 400, there are one shuntings Import 401 and two shunting outlets 402, shunting import 401 are connected to pump intake 302, are shunted and are provided with electromagnetism on guider 400 Valve 403, solenoid valve 403 is for controlling 402 break-makes of shunting outlet;Centrifugal energy nozzle 500 is arranged in unmanned plane horn end, Mei Geli Heart nozzle 500 is connected to a shunting outlet 402 respectively, and centrifugal energy nozzle 500 makes liquid carry out centrifugation sprinkling when rotating;With it is same 500 arranged for interval of multiple centrifugal energy nozzles that liquid outlet 202 is connected to is in unmanned plane circumferential direction;Control module 600 is flown for obtaining Information simultaneously passes through the break-make that flight information controls 500 start and stop of centrifugal energy nozzle and shunting outlet 402, it is preferred that flight information includes Course angle, the speed of a ship or plane and location information.
As shown in Figure 1, multi-rotor unmanned aerial vehicle according to RTK equipment calculate course angle (0~359 °), implement the speed of a ship or plane (0~ 1000cm), with reference to front position of taking off, current course angle, the speed of a ship or plane and location information in real time are calculated.Control terminal is sprayed, that is, controls mould Block by course Angle Position by being divided into four quadrants (0~359 °);Using unmanned plane head as Y-axis positive direction, nobody will be located at Horn in machine circumferential direction is divided into four quadrants, and centrifugal energy nozzle is arranged in horn end.Control module according to real time position with And course angle angle determines the start and stop of centrifugal energy nozzle and shunts the break-make of guider internal watercourses in real time.
By taking quadrotor drone as an example, each horn is located in a quadrant, i.e., each centrifugal energy nozzle is located at In one quadrant, when course angle is in 1,2 quadrant, the corresponding two centrifugal energy nozzles work of 3,4 quadrants shunts inside guider The corresponding two water routes conducting of solenoid valve control;When course angle 2,4 quadrant, the corresponding two centrifugal energy nozzles work of 1,3 quadrants, Shunt the corresponding two water routes conducting of solenoid valve control inside guider;When course angle 3,4 quadrant, 1,2 quadrants corresponding two A centrifugal energy nozzle work shunts the corresponding two water routes conducting of solenoid valve control inside guider;When course angle 1,3 quadrant, 2, the corresponding two centrifugal energy nozzles work of 4 quadrants shunts the corresponding two water routes conducting of solenoid valve control inside guide chamber.
Shaped like Fig. 3 structures, by water knockout drum 200, the water route that 100 inside of medicine-chest is drawn is divided into two-way, is separately connected pair The water pump answered, the water outlet of water pump are connected to shunting guider 400.It includes but not limited to electricity to shunt 400 internal structure of guider Magnet valve, steering engine flow dividing structure and control circuit, two shunting guiders have 4 water outlets respectively, are connected respectively to fuselage circumferential direction Four centrifugal energy nozzles at.When unmanned plane job run, water pump does not stop, by shunting guide chamber inside control mechanism into Row control, carries out water route switching.
As shown in figure 4, when the automatic flight of unmanned plane, if flying according to shape of chinese word Ji course line, when self-propulsion point 1 flies to boat Point 2, head fly towards front, and course angle is in the unlatching of 1,2 quadrants (0~179 °) rear end D, B, two nozzles, at this time solenoid valve control The both ends B, D processed water route passes through, then two nozzle of B, D is sprayed water.When by destination 2, fly to destination 3 when, course angle be in 2,4 quadrants (- 90 °~90 °) left side two nozzle of A, D opens, and solenoid valve control A, D both ends cross water, then nozzle A, D sprays water.Boat is flown to by destination 3 When point 4,3,4 quadrants (- 180 °~0) heading A, C, two nozzles are opened at course angle, and water is crossed at solenoid valve control A, C both ends, are sprayed Head A, C water spray.Other course lines are as the same.
When due to unmanned plane during flying operation, the centrifugal energy nozzle that works is always at adjacent position, and adjacent two Nozzle is connected to from the different pump housings respectively, and when aircraft executes air route switching, sprinkling system only controls nozzle and solenoid valve Switch, water pump is worked normally according to speed and preset value, and switching is all supplied water just for single water route every time, therefore is being sprayed During spilling the switching of cooperation course, remains able to ensure the accurate of flow, meet the accuracy pesticide applying function of plant protection drone.
In some embodiments, the pump housing further includes installation shell, and the pump housing is fixed on unmanned plane machine by installing shell On body.
In some embodiments, as shown in Figure 5 and Figure 6, centrifugal energy nozzle 500 according to the ... of the embodiment of the present invention, including:Drainage Disk 520, motor 510 and atomization spray disk 530.Wherein, drainage disc 520 is drained for containing (such as pesticide) liquid to be sprayed The bottom of disk 520 has outlet tube, liquid to be sprayed for being discharged.Motor 510 includes body 512, shell 513 and mounting disc 511, shell 513 is fixed on 520 top of the drainage disc, and 513 lower end of shell is equipped with the protection axle sleeve extending into drainage disc 520 514, avoid the liquid in drainage disc 520 from being contacted with motor 510;Shell 513 and mounting disc 511 limit body 512 jointly Installation space, mounting disc 511 are used to centrifugal atomizing nozzle being fixed on outer structural parts;The body 512 includes that setting exists Movement 515 in shell 513 and it is connected with the movement 515 and across the protection axle sleeve 514 to stretch out the machine of drainage disc 520 Axis 516;Motor 510 and the assembly of drainage disc 510 are compact as a result, can fully save space.
Wherein, motor 510 is preferably brshless DC motor, further, equipped with speed feedback on motor 510.
As shown in fig. 6,513 upper end opening of shell, body 512 are installed to from upper end opening in shell 513, on body 512 Arbor 516 pass through the protection of 513 lower end of shell axle sleeve 514 and movement 515 to be made to be located in shell 513,513 lower face of shell and machine 515 lower face of core is provided with threaded hole, and shell 513 and movement 515 can be attached by screw;When body 512 fixes After, it is connect with 513 upper end of shell using mounting disc 511, to close 513 upper end opening of shell, realizes the close of body 512 Envelope, while can be connect with outer structural parts by mounting disc 511.
As shown in fig. 6, atomization spray disk 530 be located at the lower section of drainage disc 520 and be provided with lead channel 535 with undertaking from it is described go out The liquid of liquid pipe discharge, and connect with the arbor 516 to drive atomization spray disk 530 to rotate.Atomization spray disk 530 and drainage disc 520 assembly is compact, can fully save space, moreover, because liquid is to be injected into atomization spray disk 530 by drainage disc 520 On, without the arbor 516 of motor 510 is processed into hollow shaft structure, thus reduce difficulty of processing and production cost.
In addition, being inserted in due to outlet tube sky in the lead channel 535 of atomization spray disk 530, i.e., there are drain gaps, so that mist Change spray disk 530 liquid can equably to be sprayed, improve fluid spills problem, outlet tube is preferably sprayed with atomization in disk 530 Heart face, so outlet tube can to atomization spray disk 530 center pour into a mould liquid so that atomization spray disk 530 can will Liquid equably sprays, and improves fluid spills problem.
In some embodiments, according to some embodiments of the present invention, as illustrated in figures 7-11, atomization spray disk 530 includes:Bottom Disk 531, multiple convex blocks 532 and multiple cylinders 533.
As shown in fig. 7, being provided with lead channel 535 in the middle part of 301 upper surface of chassis, multiple convex blocks 532 are arranged on chassis 531 Surface and circumferentially-spaced uniformly distributed at 531 edge of chassis, per two adjacent convex blocks 532 between limit a centrifugation runner 536;Multiple cylinders 533 are arranged between lead channel 536 and convex block 532, and in the multiple circumferentially-spaced of 531 upper surface of chassis It is evenly distributed with to form multiple concentric circles band of columns, all cylinders 533 limit centrifugal space 537 jointly.
It is easily understood that atomization spray disk 530 is during the work time, fluid enters lead channel 535 through exterior line, into Fluid in liquid bath 535 flows to centrifugal space 537, centrifugal space under the action of centrifugal force and its own gravity from lead channel 535 Include multiple concentric circles band of columns in 537, fluid constantly division atomization in flow process eventually forms droplet and from centrifugal space 537 enter centrifugation runner 536, then atomization spray disk 530 is discharged by centrifugation runner 536.
According to some embodiments of the present invention, as shown in figs. 10-11, atomization spray disk 530 further includes:Multiple dividing strips 534.
Uniformly at intervals in the circumferential direction of 531 upper surface of chassis, 534 part of dividing strip is located at centrifugation and flows multiple dividing strips 534 In road 536,534 remainder of dividing strip is located in centrifugal space 537, for through centrifugal space 537 segmentation after fluid into Row is divided again.
It is contemplated that as shown in figure 9, when fluid flow to the arrival end of centrifugal channel 536 from centrifugal space 537 When, dividing strip 534 is detached to that will flow out centrifugal space 537 and carry out cutting again along the droplet of centrifugation force direction flowing, from And the mist droplet particle size for entering centrifugation runner 536 is made to become smaller, after entering the segmented cutting of item 534 of droplet of centrifugation runner 536 Flow direction changes, and is divided again by 532 side wall of convex block of 536 both sides of centrifugation runner, the droplet grain for making atomization spray disk 530 be discharged Diameter smaller, sprinkling is more uniform, improves the spray effect of atomization spray disk 530.
In some embodiments, the arranged direction of each convex block 532 and the dividing strip 534 and chassis 531 are radial Unanimously.It is understood that due to atomization spray disk 530 centrifugation force direction and chassis 531 it is radially consistent, to will flow out from Heart space 537 and the droplet that centrifugal channel 536 is flow to along centrifugation force direction, it is radial on chassis 531 when being cut again, That is centrifugation force direction setting dividing strip 534 and convex block 532 can be equal with force direction when ensureing that droplet is torn by the segmentation of cylinder 533 Even distribution, atomization are more uniform.
As shown in figure 8, the atomization spray disk 530 further includes the squash type that installation nut 541 and lower end are connected with screw rod 543 Fixed hub 542,542 top outer diameter of squash type fixed hub is more than 538 outer diameter of hollow cylinder, under squash type fixed hub 542 End is connect across hollow cylinder 538 and with installation nut 541, and the arbor 516 is inserted into squash type fixed hub 542 and leads to Installation nut 541 and hollow cylinder 538 are crossed to realize the fixation of arbor 516 and atomization spray disk 530.
As shown in figure 8, installation nut 541 is located at 530 downside of atomization spray disk, squash type fixed hub 542 sprays disk from atomization 530 tops are inserted into hollow cylinder 538, and the screw rod 543 of 542 lower end of squash type fixed hub is opened from 538 bottom of hollow cylinder Mouth stretches out, and is connect with installation nut 541.Squash type fixed hub 542 includes external pressure part 544 and internal pressure containing part 545, 542 top outer diameter of squash type fixed hub is more than the outer diameter of hollow cylinder 538, i.e. the outer diameter of external pressure part 544 is more than hollow The outer diameter of cylinder 538, screw rod 543 are connected to the lower end of internal pressure containing part 545.
Therefore, as shown in figure 8, squash type fixed hub 542 is mounted on atomization spray disk 530, the machine on motor 510 When axis 516 is inserted into squash type fixed hub 542, i.e., arbor 516 is inserted into 545 center of internal pressure containing part.With installation spiral shell The locking of mother 541, the position of internal pressure containing part 545 constantly move down, while in the phase of hollow cylinder 538 and external pressure part 544 Under interaction, internal pressure containing part 545 is squeezed, and the internal diameter of internal pressure containing part 545 constantly becomes smaller, and is made in internal pressure containing part 545 Wall is gradually close to 516 outer wall of arbor, until complete the interference fit of internal pressure containing part 545 and arbor 516, realize motor 510 with The connection of atomization spray disk 530, so that motor 510 can drive atomization spray disk 530 to be rotated.
According to some embodiments of the present invention, as shown in figure 11, the two neighboring cylinder 533 being located in external circumferential The spacing for being smaller than the two neighboring cylinder 533 in inner circumferential.It is contemplated that when atomization spray disk When 530 work, the fluid in lead channel 535 flows to centrifugal space 537, includes multiple concentric circles band of columns in centrifugal space 537, when When fluid flows to the cylinder ring of innermost layer, fluid, which is divided, tears into droplet, mist droplet particle size and adjacent column on internal layer cylinder ring 533 spacing positive correlation;The spacing of adjacent column 533 is step by step when constantly outer layers cylinder ring flows droplet, on cylinder ring Reduce, be affected by this, mist droplet particle size is torn by the segmentation of cylinder 533 becomes smaller, ensures when fluid is discharged from centrifugal space 537 Mist droplet particle size, to ensure the spray effect of atomization spray disk 530.
Certainly, the present invention can also have other numerous embodiments, without deviating from the spirit and substance of the present invention, Those skilled in the art can make various corresponding change and deformations, but these corresponding changes and change according to the present invention Shape should all belong to the protection domain of appended claims of the invention.

Claims (10)

1. a kind of multi-rotor unmanned aerial vehicle sprinkling system, which is characterized in that including:
Medicine-chest is arranged on unmanned plane body, for storing liquid;
Dispenser, there are one inlets and two liquid outlets, the inlet to be connected to medicine-chest inner cavity for the dispenser tool;
The pump housing, including pump intake and pump discharge, the pump intake is connected to liquid outlet, for driving liquid medicine flow;
Guider is shunted, the shunting guider tool shunts import and pump intake there are one shunting import and two shunting outlets Connection shunts and is provided with solenoid valve on guider, and the solenoid valve is for controlling shunting outlet break-make;
Centrifugal energy nozzle, setting shunt outlet, the centrifugation with one respectively in unmanned plane horn end, each centrifugal energy nozzle Liquid is set to carry out centrifugation sprinkling when sprinkler rotation;The multiple centrifugal energy nozzle arranged for interval being connected to same liquid outlet are in unmanned plane week Upwards.
2. a kind of multi-rotor unmanned aerial vehicle sprinkling system according to claim 1, it is characterised in that:Further include control module, The control module is used to obtain flight information and controls the break-make of centrifugal energy nozzle start and stop and shunting outlet by flight information.
3. a kind of multi-rotor unmanned aerial vehicle sprinkling system according to claim 2, it is characterised in that:The flight information includes Course angle, the speed of a ship or plane and location information.
4. a kind of multi-rotor unmanned aerial vehicle sprinkling system according to claim 1, it is characterised in that:The pump housing further includes peace Shell is filled, the pump housing is fixed on by installing shell on unmanned plane body.
5. a kind of multi-rotor unmanned aerial vehicle sprinkling system according to claim 1, which is characterized in that the centrifugal energy nozzle packet It includes:
Drainage disc, the drainage disc top are equipped with inlet tube, and drainage pan bottom is equipped with outlet tube;
Motor, the motor include body, shell and mounting disc, and the shell is fixed on above the drainage disc, shell lower end Equipped with the protection axle sleeve extending into drainage disc;The shell and mounting disc limit the installation space of body, the peace jointly Sabot is used to centrifugal atomizing nozzle being fixed on outer structural parts;The body include the movement being arranged in shell and with institute Movement is stated to be connected and across the protection axle sleeve to stretch out the arbor of drainage disc;
Atomization spray disk, the atomization spray disk is located at below the drainage disc and is provided with lead channel to be arranged with accepting from the outlet tube The liquid gone out, and connect with the arbor to drive atomization spray disc spins.
6. a kind of multi-rotor unmanned aerial vehicle sprinkling system according to claim 5, which is characterized in that Pan Bao is sprayed in the atomization It includes:
Chassis, the lead channel are arranged in the middle part of chassis;
Multiple convex blocks, chassis upper surface and circumferentially-spaced uniformly distributed in chassis edge is arranged in the multiple convex block, per adjacent two A centrifugation runner is limited between a convex block;
Multiple cylinders, the multiple cylinder are arranged between lead channel and convex block, and in multiple circumferential directions of chassis upper surface between Every uniformly distributed to form multiple concentric circles band of columns, all cylinders limit centrifugal space jointly.
7. a kind of multi-rotor unmanned aerial vehicle sprinkling system according to claim 6, which is characterized in that the atomization spray disk also wraps It includes:
Multiple dividing strips, for the multiple dividing strip uniformly at intervals in the circumferential direction of chassis upper surface, dividing strip part is located at centrifugation In runner, dividing strip remainder is located in centrifugal space, for being divided again to the fluid after centrifugal space is divided.
8. a kind of multi-rotor unmanned aerial vehicle sprinkling system according to claim 6, it is characterised in that:In external circumferential The spacing for being smaller than the two neighboring cylinder in inner circumferential of the two neighboring cylinder.
9. a kind of multi-rotor unmanned aerial vehicle sprinkling system according to claim 6, it is characterised in that:It is recessed in the middle part of the chassis So that upper surface forms the lead channel, feed liquor groove center is fixed with hollow cylinder, and the hollow cylinder is for connecting arbor.
10. a kind of multi-rotor unmanned aerial vehicle sprinkling system according to claim 9, it is characterised in that:The atomization spray disk is also The squash type fixed hub of screw rod is connected with including installation nut and lower end, squash type fixed hub top outer diameter is more than open tubular column External diameter, squash type fixed hub lower end pass through hollow cylinder and are connect with installation nut, and it is solid that the arbor is inserted into squash type The fixation of arbor and atomization spray disk is realized in dead axle set and by installing nut and hollow cylinder.
CN201810230280.3A 2018-03-20 2018-03-20 A kind of multi-rotor unmanned aerial vehicle sprinkling system Pending CN108271759A (en)

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Cited By (11)

* Cited by examiner, † Cited by third party
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CN108910047A (en) * 2018-07-19 2018-11-30 苏州极目机器人科技有限公司 A kind of flusher and the unmanned plane using the flusher
CN109927894A (en) * 2019-02-28 2019-06-25 上官小珍 A kind of unmanned plane promoted based on atomizing effect
CN110979683A (en) * 2019-12-23 2020-04-10 潍坊工程职业学院 Agricultural unmanned aerial vehicle
CN111066758A (en) * 2019-12-10 2020-04-28 广东利顺科技有限公司 Many rotor unmanned aerial vehicle with centrifugal nozzle
CN112166273A (en) * 2019-11-05 2021-01-01 深圳市大疆创新科技有限公司 Solenoid valve subassembly and movable platform
CN112272758A (en) * 2019-11-04 2021-01-26 深圳市大疆创新科技有限公司 Electromagnetic flowmeter, sprinkling system and unmanned aerial vehicle
CN112334692A (en) * 2019-11-05 2021-02-05 深圳市大疆创新科技有限公司 Communicating pipe sealing assembly, electromagnetic valve assembly and movable platform
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CN113998118A (en) * 2021-11-15 2022-02-01 深圳市大疆创新科技有限公司 Unmanned aerial vehicle plant protection equipment and unmanned aerial vehicle machine carries sprinkler
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CN115889014A (en) * 2019-08-30 2023-04-04 深圳市大疆创新科技有限公司 Centrifugal spray head, spraying system and movable platform

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CN108910047B (en) * 2018-07-19 2023-12-29 极目(海南)智能育种装备有限公司 Sprinkler and unmanned aerial vehicle adopting same
CN108910047A (en) * 2018-07-19 2018-11-30 苏州极目机器人科技有限公司 A kind of flusher and the unmanned plane using the flusher
CN109927894A (en) * 2019-02-28 2019-06-25 上官小珍 A kind of unmanned plane promoted based on atomizing effect
CN115889014A (en) * 2019-08-30 2023-04-04 深圳市大疆创新科技有限公司 Centrifugal spray head, spraying system and movable platform
WO2021087677A1 (en) * 2019-11-04 2021-05-14 深圳市大疆创新科技有限公司 Solenoid valve, vehicle-mounted spraying system, and agricultural plant protection machine
CN112272758A (en) * 2019-11-04 2021-01-26 深圳市大疆创新科技有限公司 Electromagnetic flowmeter, sprinkling system and unmanned aerial vehicle
WO2021087772A1 (en) * 2019-11-05 2021-05-14 深圳市大疆创新科技有限公司 Solenoid valve assembly and movable platform
CN112334692A (en) * 2019-11-05 2021-02-05 深圳市大疆创新科技有限公司 Communicating pipe sealing assembly, electromagnetic valve assembly and movable platform
CN112166273A (en) * 2019-11-05 2021-01-01 深圳市大疆创新科技有限公司 Solenoid valve subassembly and movable platform
CN112334692B (en) * 2019-11-05 2023-10-03 深圳市大疆创新科技有限公司 Communicating pipe sealing assembly, electromagnetic valve assembly and movable platform
CN111066758B (en) * 2019-12-10 2021-06-25 广东利顺科技有限公司 Many rotor unmanned aerial vehicle with centrifugal nozzle
CN111066758A (en) * 2019-12-10 2020-04-28 广东利顺科技有限公司 Many rotor unmanned aerial vehicle with centrifugal nozzle
CN110979683B (en) * 2019-12-23 2021-06-08 潍坊工程职业学院 Agricultural unmanned aerial vehicle
CN110979683A (en) * 2019-12-23 2020-04-10 潍坊工程职业学院 Agricultural unmanned aerial vehicle
WO2022095206A1 (en) * 2020-11-09 2022-05-12 深圳市大疆创新科技有限公司 Spraying system and unmanned aerial vehicle
CN114616180A (en) * 2020-11-09 2022-06-10 深圳市大疆创新科技有限公司 Spraying system and unmanned aerial vehicle
CN113998118A (en) * 2021-11-15 2022-02-01 深圳市大疆创新科技有限公司 Unmanned aerial vehicle plant protection equipment and unmanned aerial vehicle machine carries sprinkler

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