CN111717396A - Agricultural unmanned aerial vehicle - Google Patents
Agricultural unmanned aerial vehicle Download PDFInfo
- Publication number
- CN111717396A CN111717396A CN202010631887.XA CN202010631887A CN111717396A CN 111717396 A CN111717396 A CN 111717396A CN 202010631887 A CN202010631887 A CN 202010631887A CN 111717396 A CN111717396 A CN 111717396A
- Authority
- CN
- China
- Prior art keywords
- blade
- air
- wind
- air inlet
- spraying
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- Granted
Links
- 238000005507 spraying Methods 0.000 claims abstract description 57
- 239000000463 material Substances 0.000 claims abstract description 37
- 239000007921 spray Substances 0.000 claims description 21
- 210000000056 organ Anatomy 0.000 claims description 16
- 238000007789 sealing Methods 0.000 description 5
- 230000001105 regulatory effect Effects 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000004888 barrier function Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 239000000575 pesticide Substances 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 239000011343 solid material Substances 0.000 description 1
- 239000008399 tap water Substances 0.000 description 1
- 235000020679 tap water Nutrition 0.000 description 1
Images
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
- 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
- B64U2101/00—UAVs specially adapted for particular uses or applications
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Life Sciences & Earth Sciences (AREA)
- Pest Control & Pesticides (AREA)
- Catching Or Destruction (AREA)
Abstract
The invention discloses an agricultural unmanned aerial vehicle, which belongs to the field of unmanned aerial vehicles and comprises a machine body, and a wind collecting unit and a spraying unit which are positioned on the machine body, wherein the wind collecting unit comprises a rotating arm, a first blade and a second blade, the first blade and the first blade are connected on the rotating arm, the rotating arm is connected with a central piece and can freely rotate relative to the central piece so that the first blade and the second blade can adjust the direction according to the wind direction, the outer side edges of the first blade and the second blade are respectively provided with a first air inlet and a second air inlet, the first air inlet and the second air inlet are both connected with a wind conveying unit, a first wind cavity is arranged inside the rotating arm, a second wind cavity is arranged in the central piece, the wind collecting unit is communicated with the first wind cavity, the first wind cavity is communicated with the second wind cavity, the spraying unit is provided with a material cavity, the material cavity is provided with a spraying opening, the spraying unit is further provided with a spraying pipe, one end, the other end is positioned at the spraying opening.
Description
Technical Field
The invention relates to the field of unmanned aerial vehicles.
Background
The unmanned plane is called unmanned plane for short, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device. The machine has no cockpit, but is provided with an automatic pilot, a program control device and other equipment. The personnel on the ground, the naval vessel or the mother aircraft remote control station can track, position, remotely control, telemeter and digitally transmit the personnel through equipment such as a radar. The aircraft can take off like a common airplane under the radio remote control or launch and lift off by a boosting rocket, and can also be thrown into the air by a mother aircraft for flying. During recovery, the aircraft can land automatically in the same way as the common aircraft landing process, and can also be recovered by a parachute or a barrier net for remote control. Can be repeatedly used for many times. The method is widely used for aerial reconnaissance, monitoring, communication, anti-submergence, electronic interference and the like.
Unmanned aerial vehicle also obtains more and more extensive application in the agricultural, can carry out seed scattering, the pesticide sprays by a large scale, but unmanned aerial vehicle often blocks up when spraying, wants to borrow air wind power to draw wind occasionally, but because the instability of air wind power, leads to spraying inhomogeneously.
Disclosure of Invention
The invention provides an agricultural unmanned aerial vehicle which is characterized by comprising a machine body, a wind collecting unit and a spraying unit, wherein the wind collecting unit and the spraying unit are positioned on the machine body, the machine body comprises a central piece, four connecting rods and a pair of lifting frames are respectively connected to the central piece, a propeller is arranged at the tail end of each connecting rod, the wind collecting unit comprises a rotating arm, a first blade and a second blade, the first blade and the first blade are connected to the rotating arm, the rotating arm is connected with the central piece and can freely rotate relative to the central piece so that the first blade and the second blade can adjust the direction according to the wind direction, a first air inlet and a second air inlet are respectively arranged on the outer side edges of the first blade and the second blade, the first air inlet and the second air inlet are both connected with a wind conveying unit, a first air cavity is arranged inside the rotating arm, a second air cavity is arranged in the central piece, the wind collecting unit is communicated with the first air cavity, and the second, the spraying unit is provided with a material cavity, the material cavity is provided with a spraying opening, the spraying unit is also provided with a spraying pipe, one end of the spraying pipe is communicated with the second air cavity, the other end of the spraying pipe is positioned at the spraying opening, and the air conveying unit sprays flowing wind power entering through the first air inlet and the second air inlet out of the tail end opening of the spraying pipe through the first air cavity and the second air cavity so as to drive the material in the material cavity to be sprayed out of the spraying opening; be equipped with the spring between first blade and the second blade so that first blade and second blade have opening trend, make contained angle diminish when unmanned aerial vehicle's wind-force is great between first blade and the second blade and get into collection wind unit with restriction air admission first air intake and second air intake, further restrain spray tube spun wind-force size, further make the material spray more even. The air delivery unit comprises an organ communicated with the first air inlet and the first air inlet, the organ is communicated with an air delivery pipe, one end of the air delivery pipe is connected with the wind organ, and the other end of the air delivery pipe is communicated with the first air cavity. And the second wind cavity is provided with a regulator for regulating wind power so as to regulate resistance. The edges of the first air inlet and the second air inlet are provided with a first wind collecting plate and a second wind collecting plate so that enough wind power can enter the first air inlet and the second air inlet. Two ends of the organ are communicated with the first air inlet and the second air inlet, and the middle of the organ is communicated with the air delivery pipe.
The top section of the first blade and the second blade is a triangular structure.
Drawings
Figure 1 is a schematic view of the drone of the present invention;
FIG. 2 is a schematic view of a wind collection unit and a spray unit;
FIG. 3 is a schematic view of a spray unit;
FIG. 4 is a schematic view of a wind collection unit;
FIG. 5 is a schematic view of a first blade and a second blade;
FIG. 6 is a schematic view of a preferred spray unit;
FIG. 7 is a schematic view of a motor;
the labels in the figure are: 1-labeled in the figure: 100-machine body, 110-propeller, 120-connecting rod, 130-lifting frame, 140-central piece, 141-second air cavity, 142-regulator, 200-wind collecting unit, 210-rotating arm, 220-first air cavity, 230-first blade, 231-first air inlet, 232-first wind collecting plate, 240-second blade, 241-second air inlet, 242-second wind collecting plate, 250-wind conveying unit, 251-organ, 252-wind conveying pipe, 300-spraying unit, 310-spraying opening, 320-spraying pipe, 330-connecting plate, 340-fixing plate, 350-motor, 360-driving shaft, 370-arc plate, 380-material cavity, 390-sealing plate and 400-rotating shaft.
Detailed Description
The present invention will be described in detail below with reference to the accompanying drawings.
As shown in fig. 1, the invention discloses an agricultural unmanned aerial vehicle, which comprises a machine body 100, and a wind collecting unit 200 and a spraying unit 300 which are positioned on the machine body 100, wherein the machine body 100 comprises a central piece 140, the central piece is respectively connected with four connecting rods 120 and a pair of lifting frames 130, the tail ends of the connecting rods are provided with propellers 100, the propellers 100 provide flying power for the unmanned aerial vehicle, the central piece is a main frame part of the unmanned aerial vehicle, and components such as a controller, a power supply and the like are arranged in the central piece. The air collecting unit collects air flow above the unmanned aerial vehicle and conveys the air flow to the spraying unit 300 to provide certain spraying power for the spraying unit, as shown in fig. 3, the spraying unit is provided with a material cavity 380, the material cavity is provided with a spraying opening 310, the spraying unit is also provided with a spraying pipe 320, the collected air flow is sprayed out through the tail end of the spraying pipe opening, and then the material in the material cavity is guided to be sprayed out, the spraying speed of the material in the spraying mode is related to the size of the air flow, the larger the air flow is, the faster the material spraying speed is, and the larger the air flow speed is, the larger the air flow speed is, the smaller the air flow sprayed out by the spraying pipe is, so that the spraying is influenced by the air flow, and the spraying is not uniform.
Therefore, in the improved scheme, the wind collecting unit includes a rotating arm 210, a first blade 230, and a second blade 240, the first blade and the first blade are connected to the rotating arm 210, the rotating arm and the center piece are connected 140 and can freely rotate (rotate around a shaft 400 as shown in fig. 4) relative to the center piece, a bearing can be disposed between the specific rotating arm and the center piece, so that the first blade and the second blade can adjust the direction according to the wind direction, so that wind can be collected all the time regardless of the wind direction, the outer sides of the first blade and the second blade are respectively provided with a first wind inlet 231 and a second wind inlet 241, the first wind inlet and the second wind inlet are both connected with the wind conveying unit 250, the first wind cavity 220 is disposed inside the rotating arm, the second wind cavity 141 is disposed in the center piece, the wind collecting unit is communicated with the first wind cavity, the first wind cavity is communicated with the second wind cavity, the spraying unit is provided with a material cavity 380, the material cavity is provided with a spraying opening 310, the spraying unit is also provided with a spraying pipe 320, one end of the spraying pipe is communicated with the second air cavity, the other end of the spraying pipe is positioned at the spraying opening, and the air conveying unit sprays flowing wind power entering through the first air inlet and the second air inlet out of the tail end opening of the spraying pipe through the first air cavity and the second air cavity so as to drive the material in the material cavity to be sprayed out of the spraying opening;
be equipped with the spring between first blade and the second blade so that first blade and second blade have opening trend, make contained angle diminish when unmanned aerial vehicle's wind-force is great between first blade and the second blade and get into collection wind unit with restriction air admission first air intake and second air intake, further restrain spray tube spun wind-force size, further make the material spray more even.
In a preferred embodiment, the air delivery unit 250 includes an organ 251 communicated with the first air inlet and the first air inlet, the organ is communicated with an air delivery pipe 252, one end of the air delivery pipe is connected with the organ, and the other end of the air delivery pipe is communicated with the first air cavity. The organ is elastic and can adapt to the change of an included angle between the first blade and the second blade, two ends of the organ are communicated with the first air inlet and the second air inlet, and the middle of the organ is communicated with the air delivery pipe (252).
In a preferred embodiment, the second wind chamber is provided with a regulator 142 for regulating wind force to adjust the resistance, which is similar to the existing structure for regulating tap water, and is mainly adjusted by increasing or decreasing the resistance. When larger materials are needed for some scattering, the resistance adjusted by the adjuster 142 is small to increase the size of the air ejected and increase the scattering density.
In a preferred scheme, the edges of the first air inlet and the second air inlet are provided with a first wind collecting plate and a second wind collecting plate so as to enable enough wind power to enter the first air inlet and the second air inlet, and mainly enable the wind power entering the air inlets to be large so as to provide enough power for spreading.
In a preferred embodiment, the first and second blades have a triangular cross-section as shown in fig. 5.
In a modified embodiment, as shown in fig. 2, the end of the nozzle 320 is provided with two connecting plates 330, the two connecting plates 330 are symmetrically arranged, the connecting plates 330 are arranged to be thin to prevent the material from scattering, and the connecting plates can also be arranged to be thin column-shaped structures, and are usually made of metal materials such as iron. The two connecting plates are jointly connected with a fixing plate 340, the fixing plate 340 is of a plate-shaped structure, the preferential setting is a circular plate, the fixing plate is provided with a motor 350, the motor 350 is positioned on the lower side surface of the fixing plate 340, the motor 350 can be remotely controlled, the motor 350 is driven to be connected with a driving shaft 360, the driving shaft is connected with the motor 350 and driven to rotate by the motor 350, the tail end of the driving shaft is connected with an arc plate 370, the arc plate 370 is fixedly connected with the driving shaft, the arc plate is provided with a concave surface and a convex surface, the concave surface faces downwards, the convex surface faces upwards, the arc plate is positioned between the two connecting plates 330, a sealing plate 390 is connected on the spray nozzle, the sealing plate is hinged with the spray nozzle, the hinged part is a hinged shaft, the sealing plate can rotate relative to the hinged shaft to open or seal the spray nozzle, a spring is arranged on the hinged, and then make the material impact of material chamber on the arc convex surface through spray tube spun air current, the arc can be rotated by motor drive, and then with the material scattering all around. The material is solid material seed. The nozzle passes through the material chamber 380, and the end of the nozzle is located in the spray opening. In the modified unit that sprays, the closing plate will spray the mouth sealed under the elasticity effect under the natural state, the material can not fall down, unmanned aerial vehicle rises to the air the back, long-range regulator 142 of opening, the air current is followed the spray tube blowout, the air current makes the closing plate open, the material falls down, and under the drive of air current, strike arc 370 surface, wherein the rotation rate of different positions on the arc is different (marginal velocity is big), make the impact force of the arc that strikes the above-mentioned material and receive different, the speed of material scattering is different, what the speed is big scatters is farther, what the speed is little scatters more, make scattering more even, the radiating area is big, and the flow of material whereabouts can be adjusted its 142 control, the resistance is smaller, the material flows greatly, jet density is big. The invention does not need a separate switch device, and the sealing plate can be automatically opened when the air flow is opened, thereby having simple structure.
Claims (6)
1. The agricultural unmanned aerial vehicle is characterized by comprising a machine body (100), a wind collecting unit (200) and a spraying unit (300), wherein the wind collecting unit (200) and the spraying unit (300) are positioned on the machine body (100), the machine body (100) comprises a center piece (140), four connecting rods (120) and a pair of lifting frames (130) are respectively connected to the center piece, a propeller (100) is arranged at the tail end of each connecting rod, the wind collecting unit comprises a rotating arm (210), a first blade (230) and a second blade (240), the first blade and the first blade are connected to the rotating arm (210), the rotating arm and the center piece are connected (140) and can freely rotate relative to the center piece so that the first blade and the second blade can adjust the direction according to the wind direction, a first air inlet (231) and a second air inlet (241) are respectively arranged on the outer side of the first blade and the outer side of the second blade, and the first air inlet and the second, a first air cavity (220) is formed in the rotating arm, a second air cavity (141) is formed in the central piece, an air collecting unit is communicated with the first air cavity, the first air cavity is communicated with the second air cavity, a material cavity (380) is formed in the spraying unit, a spraying opening (310) is formed in the material cavity, a spraying pipe (320) is further arranged in the spraying unit, one end of the spraying pipe is communicated with the second air cavity, the other end of the spraying pipe is located at the spraying opening, and the air conveying unit sprays flowing wind power entering through the first air inlet and the second air inlet out of the tail end opening of the spraying pipe through the first air cavity and the second air cavity so as to drive materials in the material cavity to be sprayed out of the spraying;
be equipped with the spring between first blade and the second blade so that first blade and second blade have opening trend, make contained angle diminish when unmanned aerial vehicle's wind-force is great between first blade and the second blade and get into collection wind unit with restriction air admission first air intake and second air intake, further restrain spray tube spun wind-force size, further make the material spray more even.
2. An agricultural unmanned aerial vehicle according to claim 1, wherein the air delivery unit (250) comprises an organ (251) communicated with the first air inlet and the first air inlet, the organ is communicated with an air delivery pipe (252), one end of the air delivery pipe is connected with the air organ, and the other end of the air delivery pipe is communicated with the first air cavity.
3. An agricultural drone according to claim 2, characterised in that the second wind chamber is provided with a regulator (142) to regulate the wind force to regulate the drag.
4. An agricultural unmanned aerial vehicle according to claim 3, wherein the first air inlet and the second air inlet are provided with a first wind collecting plate and a second wind collecting plate at edges thereof so that sufficient wind force can enter the first air inlet and the second air inlet.
5. An agricultural unmanned aerial vehicle according to claim 4, wherein two ends of the organ are communicated with the first air inlet and the second air inlet, and the middle of the organ is communicated with the air delivery pipe (252).
6. An agricultural drone according to claim 5, wherein the first and second blades are triangular in plan section.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010631887.XA CN111717396B (en) | 2020-07-03 | 2020-07-03 | Agricultural unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010631887.XA CN111717396B (en) | 2020-07-03 | 2020-07-03 | Agricultural unmanned aerial vehicle |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN111717396A true CN111717396A (en) | 2020-09-29 |
| CN111717396B CN111717396B (en) | 2021-06-11 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202010631887.XA Active CN111717396B (en) | 2020-07-03 | 2020-07-03 | Agricultural unmanned aerial vehicle |
Country Status (1)
| Country | Link |
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| CN (1) | CN111717396B (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103661946A (en) * | 2013-12-13 | 2014-03-26 | 江苏大学 | Flow diversion anti-drifting devices for rotary-wing unmanned plane mist spraying |
| CN106275440A (en) * | 2016-08-31 | 2017-01-04 | 宁夏大学 | Storehouse is hung in a kind of unmanned plane many positions in storehouse plant seeds by airplane |
| CN209650552U (en) * | 2019-03-12 | 2019-11-19 | 四川极云智飞科技有限公司 | A kind of air inducing sows unmanned plane |
| EP3620040A1 (en) * | 2018-09-05 | 2020-03-11 | Bourgault Industries Ltd. | Seed inductor apparatus |
| CN210175129U (en) * | 2019-05-27 | 2020-03-24 | 安阳全丰航空植保科技股份有限公司 | Agricultural unmanned aerial vehicle granule jettison device |
-
2020
- 2020-07-03 CN CN202010631887.XA patent/CN111717396B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103661946A (en) * | 2013-12-13 | 2014-03-26 | 江苏大学 | Flow diversion anti-drifting devices for rotary-wing unmanned plane mist spraying |
| CN106275440A (en) * | 2016-08-31 | 2017-01-04 | 宁夏大学 | Storehouse is hung in a kind of unmanned plane many positions in storehouse plant seeds by airplane |
| EP3620040A1 (en) * | 2018-09-05 | 2020-03-11 | Bourgault Industries Ltd. | Seed inductor apparatus |
| CN209650552U (en) * | 2019-03-12 | 2019-11-19 | 四川极云智飞科技有限公司 | A kind of air inducing sows unmanned plane |
| CN210175129U (en) * | 2019-05-27 | 2020-03-24 | 安阳全丰航空植保科技股份有限公司 | Agricultural unmanned aerial vehicle granule jettison device |
Also Published As
| Publication number | Publication date |
|---|---|
| CN111717396B (en) | 2021-06-11 |
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| TA01 | Transfer of patent application right |
Effective date of registration: 20210520 Address after: No.276 shanxiali, Punan village, Pengjie Town, Luqiao District, Taizhou City, Zhejiang Province 318050 Applicant after: Chen Guoyun Address before: No. 196, Dangui street, Ziliujing District, Zigong City, Sichuan Province Applicant before: He Daan |
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Effective date of registration: 20230620 Address after: 272400 Room 501, building B3, xishengxiang Town, nanjiacheng Road, Chengxiang Avenue, Jining Economic Development Zone, Jining City, Shandong Province Patentee after: Shandong Tonghui Intelligent Technology Co.,Ltd. Address before: No.276 shanxiali, Punan village, Pengjie Town, Luqiao District, Taizhou City, Zhejiang Province 318050 Patentee before: Chen Guoyun |
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