CN107117297A - A kind of multi-rotor aerocraft for pesticide spraying - Google Patents
A kind of multi-rotor aerocraft for pesticide spraying Download PDFInfo
- Publication number
- CN107117297A CN107117297A CN201710314425.3A CN201710314425A CN107117297A CN 107117297 A CN107117297 A CN 107117297A CN 201710314425 A CN201710314425 A CN 201710314425A CN 107117297 A CN107117297 A CN 107117297A
- Authority
- CN
- China
- Prior art keywords
- aircraft body
- pesticide spraying
- aircraft
- water tank
- rotor aerocraft
- 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
Links
- 239000000575 pesticide Substances 0.000 title claims abstract description 25
- 238000005507 spraying Methods 0.000 title claims abstract description 25
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 69
- 238000003780 insertion Methods 0.000 claims abstract description 9
- 230000037431 insertion Effects 0.000 claims abstract description 9
- 230000001681 protective effect Effects 0.000 claims description 10
- 230000005611 electricity Effects 0.000 claims description 4
- 239000003905 agrochemical Substances 0.000 abstract description 7
- 238000010438 heat treatment Methods 0.000 abstract description 5
- 238000012545 processing Methods 0.000 abstract description 5
- 238000013461 design Methods 0.000 abstract description 4
- 230000000694 effects Effects 0.000 abstract description 4
- 238000000034 method Methods 0.000 abstract description 2
- 238000010586 diagram Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000002360 preparation method Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 239000008236 heating water Substances 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000000361 pesticidal effect Effects 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
-
- 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; ARRANGEMENTS 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
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/24—Aircraft characterised by the type or position of power plant using steam, electricity, or spring force
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Abstract
The invention discloses a kind of multi-rotor aerocraft for pesticide spraying, including aircraft body, the aircraft body is made up of the multiple equally distributed balance rotors for being arranged on the aircraft body side and the water tank for being arranged on the aircraft body bottom, the top of the aircraft body is provided with battery case, and the battery case insertion is arranged in the aircraft body, this kind is used for the multi-rotor aerocraft of pesticide spraying, change mode of the conventional aircraft battery box design in aircraft body bottom, battery case is embedded in the top for being arranged on aircraft body, be conducive to having a smooth flight property of the lifting for the multi-rotor aerocraft of pesticide spraying, the side of water tank is provided with water quality heater, micro- heat can be carried out to water body between water body enters water tank, not only contribute to reduce the procedure of processing of water body early stage, and the water body of micro- heating can be preferably melt and dissolved with agricultural chemicals, improve the effect of agricultural chemicals.
Description
Technical field
The present invention relates to vehicle technology field, specially a kind of multi-rotor aerocraft for pesticide spraying.
Background technology
So-called aircraft, aircraft (flightvehicle) be manufactured by the mankind, can fly away from ground, in space flight simultaneously
The flying object controlled by people, in existing flying object, the multi-rotor aerocraft with VTOL and hovering ability has
Application field widely, its compared with traditional single-rotor helicopter, with it is simple in construction, safeguard easily, blade killing
Power is small, safe operation the characteristics of, the effect become more and more important is not only played in military field, also photography in the air, agricultural plant protection,
Multiple civil areas such as power-line patrolling, traffic tour and Disaster Assessment are widely used.
But existing aircraft, more designs battery case in the bottom of aircraft, in the flight course of aircraft, easily
The unstable phenomenon of generation causes to drop, when water tank add water processing, because water tank does not have preheating equipment to carry out at heating
Reason, the early stage procedure of processing increase of water body is not only resulted in, and the melt and dissolved property between water body and agricultural chemicals is poor, and pesticidal effects cannot
Embody.
So, how to design a kind of multi-rotor aerocraft for pesticide spraying, the problem of currently being solved as us.
The content of the invention
It is an object of the invention to provide a kind of multi-rotor aerocraft for pesticide spraying, to solve above-mentioned background technology
The problem of middle proposition.
To achieve the above object, the present invention provides following technical scheme：A kind of multi-rotor aerocraft for pesticide spraying,
Including aircraft body, the aircraft body is by being arranged on multiple equally distributed balance rotors of the aircraft body side
And the water tank composition of the aircraft body bottom is arranged on, the top of the aircraft body is provided with battery case, and the electricity
Pond box insertion is arranged in the aircraft body, and the side of the battery case is provided with multiple equally distributed power lines, and
The power line is electrically connected with battery case, and the side of the aircraft body is provided with signal receiver, the aircraft sheet
The inside of body is provided with airduct, and the aircraft body is closely welded with airduct, and the side of the water tank is provided with feeder,
And the feeder is fixedly connected with water tank, the side of the feeder is provided with spiral cap, the spiral cap and charging
Device is flexibly connected, and the side of the water tank is provided with water inlet pipe, and the bottom of the water tank is provided with pneumatic turntable, and described pneumatic
Turntable is flexibly connected with water tank, and the side of the pneumatic turntable is provided with multiple equally distributed sprinklers, the sprinkler with
Pneumatic turntable is fixedly connected, and the bottom of the aircraft body is provided with multiple equally distributed support foot rests, and the support
Foot stool is fixedly connected with aircraft body, and the side of the aircraft body is provided with multiple equally distributed horns, the machine
The side of arm is mounted on protective boot, and the bottom of the balance rotor is mounted on stepper motor.
Further, the bottom of the signal receiver is provided with coiling locator, and the signal receiver and flight
Device body is flexibly connected by coiling locator.
Further, the side of the protective boot is mounted on screens device, and the screens device insertion is arranged on described anti-
Protect in gum cover, and be fixedly connected with the horn.
Further, the side of the balance rotor is provided with live bearing, and the balance rotor leads to stepper motor
Cross live bearing flexible connection.
Further, the inside of the aircraft body is provided with JK equilibristats, and the JK equilibristats and aircraft sheet
Body is electrically connected with.
Further, the side of the water inlet pipe is provided with water quality heater, and water quality heater insertion is arranged on
In the aircraft body, and it is fixedly connected with the water inlet pipe.
Compared with prior art, the beneficial effects of the invention are as follows：This kind is used for the multi-rotor aerocraft of pesticide spraying, changes
Battery case is embedded in the top for being arranged on aircraft body by conventional aircraft battery box design in the mode of aircraft body bottom
End, is conducive to having a smooth flight property of the lifting for the multi-rotor aerocraft of pesticide spraying, and the side of water tank is provided with water quality heating
Device, can carry out micro- processing step for heating, not only contributing to reduce water body early stage between water body enters water tank to water body
Suddenly, and micro- heating water body and agricultural chemicals can preferably it is melt and dissolved, improve agricultural chemicals effect.
Brief description of the drawings
Fig. 1 is the overall structure diagram of the present invention；
Fig. 2 is the water tank partial structural diagram of the present invention；
Fig. 3 is the JK equilibristat partial structural diagrams of the present invention；
In figure：1- balances rotor；2- live bearings；3- stepper motors；4- horns；5- support foot rests；6- protective boots；7-
Screens device；8- water tanks；9- power lines；10- feeders；11- spiral caps；12- aircraft bodies；13- coiling locators；14-
Signal receiver；15- water inlet pipes；16- battery cases；17- water quality heaters；18- sprinklers；The pneumatic turntables of 19-；20-JK is balanced
Instrument；21- airducts.
Embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Site preparation is described, it is clear that described embodiment is only a part of embodiment of the invention, rather than whole embodiments.It is based on
Embodiment in the present invention, it is every other that those of ordinary skill in the art are obtained under the premise of creative work is not made
Embodiment, belongs to the scope of protection of the invention.
Fig. 1-3 are referred to, the present invention provides a kind of technical scheme：A kind of multi-rotor aerocraft for pesticide spraying, bag
Include aircraft body 12, the aircraft body 12 is by being arranged on multiple equally distributed balances of the side of aircraft body 12
Rotor 1 and it is arranged on the water tank 8 of the bottom of aircraft body 12 and constitutes, the top of the aircraft body 12 is provided with battery case
16, and the insertion of the battery case 16 is arranged in the aircraft body 12, the side of the battery case 16 be provided with it is multiple
The power line 9 of even distribution, and the power line 9 is electrically connected with battery case 16, the side of the aircraft body 12 is provided with
Signal receiver 14, the inside of the aircraft body 12 is provided with airduct 21, and the aircraft body 12 and airduct 21 are tight
Close welding, the side of the water tank 8 is provided with feeder 10, and the feeder 10 is fixedly connected with water tank 8, the feeder
10 side is provided with spiral cap 11, and the spiral cap 11 is flexibly connected with feeder 10, and the side of the water tank 8 is installed
There is water inlet pipe 15, the bottom of the water tank 8 is provided with pneumatic turntable 19, and the pneumatic turntable 19 is flexibly connected with water tank 8, institute
The side for stating pneumatic turntable 19 is provided with multiple equally distributed sprinklers 18, and the sprinkler 18 is fixed with pneumatic turntable 19 to be connected
Connect, the bottom of the aircraft body 12 is provided with multiple equally distributed support foot rests 5, and the support foot rest 5 and flight
Device body 12 is fixedly connected, and the side of the aircraft body 12 is provided with multiple equally distributed horns 4, the horn 4
Side is mounted on protective boot 6, and the bottom of the balance rotor 1 is mounted on stepper motor 3, and the stepper motor 3 has
Power is steadily preferably passed to, is conducive to ensureing the smooth flight of the multi-rotor aerocraft for pesticide spraying.
Further, the bottom of the signal receiver 14 is provided with coiling locator 13, and the signal receiver 14
It is flexibly connected with aircraft body 12 by coiling locator 13, facilitates the activity of signal receiver 14, is conducive to increase to believe
The signal range of receiving of number receiver 14.
Further, the side of the protective boot 6 is mounted on screens device 7, and the insertion of screens device 7 is arranged on described
In protective boot 6, and it is fixedly connected with the horn 4, strengthens protective boot 6, is conducive to extending the usage cycles of horn 4.
Further, the side of the balance rotor 1 is provided with live bearing 2, and the balance rotor 1 and stepper motor
3 are flexibly connected by live bearing 2, the rotation of the balance rotor 1, effectively can be provided rotation for aircraft body 12 and be risen
Power.
Further, the inside of the aircraft body 12 is provided with JK equilibristats 20, and the JK equilibristats 20 are with flying
Row device body 12 is electrically connected with, and accelerates the circuit transmission speed of aircraft body 12, is conducive to improving aircraft body 12
Operating efficiency.
Further, the side of the water inlet pipe 15 is provided with water quality heater 17, and the water quality heater 17 is embedded in
It is arranged in the aircraft body 12, and is fixedly connected with the water inlet pipe 15, makes water quality heater 17 more firm, favorably
In the service life of extension water quality heater 17.
Operation principle：First, user of service is by the battery case 16 on the top of aircraft body 12, and battery, which is put into, to be used for
The inside of the multi-rotor aerocraft of pesticide spraying, power line 9 is that aircraft body 12 connects circuit, and aircraft body 12, which enters, to be treated
Machine state, now opens the spiral cap 11 of the side of water tank 8, is that water tank 8 carries out agricultural chemicals addition by feeder 10, then pass through water
The water inlet pipe 15 of the opposite side of case 8 is that water tank carries out the processing that adds water, and water body is entered before water tank 8, and water quality heater 17 connects electricity
Road, after the completion of carrying out micro- heating, preparation to water body, the signal receiver that user of service passes through the side of aircraft body 12
14, it is connected signal is carried out for the multi-rotor aerocraft of pesticide spraying and terminal, terminal signal instruction hair
After going out, the multi-rotor aerocraft for pesticide spraying, which is proceeded by, to be used, in use, and aircraft body 12 is to stepping electricity
Machine 3 transmits electric current, and stepper motor 3 is connected after circuit, converts electrical energy into mechanical energy, is carried by live bearing 2 for balance rotor 1
For rotatory force, after balance rotor 1 rotate at a high speed, aircraft body 12 is driven to go up to the air, and according to signal instruction, flight is to needing to spray
Spill in the region of agricultural chemicals, flight course, the flight that JK equilibristats 20 increase the multi-rotor aerocraft for pesticide spraying automatically is put down
Stability, is reached behind pesticide spraying region, random rotation takes place in the pneumatic turntable 19 of the bottom of water tank 8 under the blowing of wind,
Now sprinkler 18 proceeds by pesticide spraying.
Although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of changes, modification can be carried out to these embodiments, replace without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (6)
1. a kind of multi-rotor aerocraft for pesticide spraying, including aircraft body (12), it is characterised in that：The aircraft
Body (12) is by being arranged on multiple equally distributed balance rotors (1) of aircraft body (12) side and being arranged on the flight
The water tank (8) of device body (12) bottom is constituted, and the top of the aircraft body (12) is provided with battery case (16), and the electricity
Pond box (16) insertion is arranged in the aircraft body (12), and the side of the battery case (16) is provided with multiple be uniformly distributed
Power line (9), and the power line (9) and battery case (16) be electrically connected with, and the side of the aircraft body (12) is installed
There is signal receiver (14), the inside of the aircraft body (12) is provided with airduct (21), and the aircraft body (12)
Closely welded with airduct (21), the side of the water tank (8) is provided with feeder (10), and the feeder (10) and water tank
(8) it is fixedly connected, the side of the feeder (10) is provided with spiral cap (11), the spiral cap (11) and feeder
(10) it is flexibly connected, the side of the water tank (8) is provided with water inlet pipe (15), and the bottom of the water tank (8) is provided with pneumatic turn
Platform (19), and the pneumatic turntable (19) is flexibly connected with water tank (8), the side of the pneumatic turntable (19) be provided with it is multiple
The sprinkler (18) of even distribution, the sprinkler (18) is fixedly connected with pneumatic turntable (19), the aircraft body (12)
Bottom is provided with multiple equally distributed support foot rests (5), and the support foot rest (5) and the fixed company of aircraft body (12)
Connect, the side of the aircraft body (12) is provided with multiple equally distributed horns (4), and the side of the horn (4) is pacified
Equipped with protective boot (6), the bottom of the balance rotor (1) is mounted on stepper motor (3).
2. a kind of multi-rotor aerocraft for pesticide spraying according to claim 1, it is characterised in that：The signal connects
The bottom for receiving device (14) is provided with coiling locator (13), and the signal receiver (14) and aircraft body (12) by around
Line locator (13) is flexibly connected.
3. a kind of multi-rotor aerocraft for pesticide spraying according to claim 1, it is characterised in that：The protective rubber
The side of set (6) is mounted on screens device (7), and screens device (7) insertion is arranged in the protective boot (6), and with institute
Horn (4) is stated to be fixedly connected.
4. a kind of multi-rotor aerocraft for pesticide spraying according to claim 1, it is characterised in that：The balance rotation
The side of the wing (1) is provided with live bearing (2), and the balance rotor (1) and stepper motor (3) are living by live bearing (2)
Dynamic connection.
5. a kind of multi-rotor aerocraft for pesticide spraying according to claim 1, it is characterised in that：The aircraft
The inside of body (12) is provided with JK equilibristats (20), and the JK equilibristats (20) are electrically connected with aircraft body (12).
6. a kind of multi-rotor aerocraft for pesticide spraying according to claim 1, it is characterised in that：The water inlet pipe
(15) side is provided with water quality heater (17), and the water quality heater (17) insertion is arranged on the aircraft body
(12) in, and it is fixedly connected with the water inlet pipe (15).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710314425.3A CN107117297A (en) | 2017-05-06 | 2017-05-06 | A kind of multi-rotor aerocraft for pesticide spraying |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710314425.3A CN107117297A (en) | 2017-05-06 | 2017-05-06 | A kind of multi-rotor aerocraft for pesticide spraying |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107117297A true CN107117297A (en) | 2017-09-01 |
Family
ID=59727687
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710314425.3A Pending CN107117297A (en) | 2017-05-06 | 2017-05-06 | A kind of multi-rotor aerocraft for pesticide spraying |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107117297A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107608383A (en) * | 2017-10-13 | 2018-01-19 | 南京涵曦月自动化科技有限公司 | A kind of multi-rotor unmanned aerial vehicle auto-controller sprayed insecticide |
| CN108216616A (en) * | 2018-01-23 | 2018-06-29 | 焦作大学 | A kind of efficient unmanned plane automatic adjustment rotor structure |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104768847A (en) * | 2012-09-19 | 2015-07-08 | 太阳方舟公司 | Hydrogen-regenerating solar-powered aircraft |
| JP5890569B1 (en) * | 2015-08-12 | 2016-03-22 | ヒロボー株式会社 | Multi-rotor type helicopter and method of spraying medicine using the same |
| CN206914630U (en) * | 2017-05-06 | 2018-01-23 | 安徽省先胜农业发展有限公司 | A kind of multi-rotor aerocraft for pesticide spraying |
-
2017
- 2017-05-06 CN CN201710314425.3A patent/CN107117297A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104768847A (en) * | 2012-09-19 | 2015-07-08 | 太阳方舟公司 | Hydrogen-regenerating solar-powered aircraft |
| JP5890569B1 (en) * | 2015-08-12 | 2016-03-22 | ヒロボー株式会社 | Multi-rotor type helicopter and method of spraying medicine using the same |
| CN206914630U (en) * | 2017-05-06 | 2018-01-23 | 安徽省先胜农业发展有限公司 | A kind of multi-rotor aerocraft for pesticide spraying |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107608383A (en) * | 2017-10-13 | 2018-01-19 | 南京涵曦月自动化科技有限公司 | A kind of multi-rotor unmanned aerial vehicle auto-controller sprayed insecticide |
| CN107608383B (en) * | 2017-10-13 | 2021-01-08 | 南京涵曦月自动化科技有限公司 | Multi-rotor unmanned aerial vehicle automatic control instrument for spraying pesticides |
| CN108216616A (en) * | 2018-01-23 | 2018-06-29 | 焦作大学 | A kind of efficient unmanned plane automatic adjustment rotor structure |
| CN108216616B (en) * | 2018-01-23 | 2021-03-30 | 焦作大学 | High-efficient unmanned aerial vehicle automatically regulated rotor structure |
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| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| AD01 | Patent right deemed abandoned | ||
| AD01 | Patent right deemed abandoned |
Effective date of abandoning: 20231229 |