CN109315378A - The dynamic mixed intelligent fog machine of the more rotor fuels of single-track - Google Patents
The dynamic mixed intelligent fog machine of the more rotor fuels of single-track Download PDFInfo
- Publication number
- CN109315378A CN109315378A CN201811205221.7A CN201811205221A CN109315378A CN 109315378 A CN109315378 A CN 109315378A CN 201811205221 A CN201811205221 A CN 201811205221A CN 109315378 A CN109315378 A CN 109315378A
- Authority
- CN
- China
- Prior art keywords
- rotor
- machine
- cockpit
- fuels
- fog machine
- 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
- 239000000446 fuel Substances 0.000 title claims abstract description 15
- 239000007921 spray Substances 0.000 claims abstract description 8
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims abstract description 4
- 239000007788 liquid Substances 0.000 claims description 10
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 9
- 230000000694 effects Effects 0.000 claims description 6
- 239000000969 carrier Substances 0.000 claims description 3
- 238000010276 construction Methods 0.000 abstract description 3
- 230000001066 destructive effect Effects 0.000 abstract description 2
- 239000003814 drug Substances 0.000 description 4
- 239000012530 fluid Substances 0.000 description 3
- 241000196324 Embryophyta Species 0.000 description 2
- 238000000889 atomisation Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 239000003595 mist Substances 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 229940079593 drug Drugs 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000001802 infusion Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 210000000056 organ Anatomy 0.000 description 1
- 238000010248 power generation Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 230000032258 transport Effects 0.000 description 1
Classifications
-
- A—HUMAN NECESSITIES
- A01—AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
- A01M—CATCHING, TRAPPING OR SCARING OF ANIMALS; APPARATUS FOR THE DESTRUCTION OF NOXIOUS ANIMALS OR NOXIOUS PLANTS
- A01M7/00—Special adaptations or arrangements of liquid-spraying apparatus for purposes covered by this subclass
- A01M7/0025—Mechanical sprayers
- A01M7/0032—Pressure sprayers
- A01M7/0042—Field sprayers, e.g. self-propelled, drawn or tractor-mounted
-
- A—HUMAN NECESSITIES
- A01—AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
- A01M—CATCHING, TRAPPING OR SCARING OF ANIMALS; APPARATUS FOR THE DESTRUCTION OF NOXIOUS ANIMALS OR NOXIOUS PLANTS
- A01M7/00—Special adaptations or arrangements of liquid-spraying apparatus for purposes covered by this subclass
- A01M7/0082—Undercarriages, frames, mountings, couplings, tanks
Abstract
A kind of dynamic mixed intelligent fog machine of the more rotor fuels of single-track, including flight support main body；Wind-force pressure exerting arrangement is equipped on the flight support body top rotor bracket, equipped with cockpit in the rotor bracket, split type medicine-chest is equipped at left and right sides of the cockpit, intelligent control center is mounted in the cockpit pedestal, the two sides of bottom case are vertically installed with transfusion pole outside the intelligent control center, and there are several spray heads for the transfusion pole bottom.The present invention is a kind of landing-type fog machine, using the motion mode of single wheel single track, solves the occupied area for reducing value preserving machine, while also reducing value preserving machine own wt, reduces the destructive rate of ridge.Built-in rotor balance system solves the technical issues of fuselage inclination.Brief body construction is more suitable for unmanned.
Description
Technical field
The present invention relates to fog machine, the dynamic mixed intelligent fog machine of especially a kind of more rotor fuels of single-track.
Background technique
Fog machine is the essential Work machine of modern agriculture, with the development of the times and technological progress, various
Equipment for plant protection continuing to bring out, can substantially divide two major classes, first is that self-propelled, second is that unmanned plane formula (single rotor or more rotors)；
Dry field machinery comparative maturity, but not more satisfactory equipment paddy field machine occurs.China is vast in territory, populous, paddy field
Cultivated area is very huge, so a ideal paddy field machine of invention is significantly.
Summary of the invention
The technical problem to be solved in the invention is that the present invention provides a kind of cruise duration is long, medicine mist spraying swath is wide, can collect
At the dynamic mixed intelligent fog machine of more rotor fuels of broadcast application additional facilities.
In order to solve the above technical problems, the present invention provides a kind of dynamic mixed intelligent fog machine of the more rotor fuels of single-track, packets
Include flight support main body；Wind-force pressure exerting arrangement, the rotor bracket are equipped on the flight support body top rotor bracket
It is interior equipped with cockpit, be equipped with split type medicine-chest at left and right sides of the cockpit, be mounted with intelligence in the cockpit pedestal
Control centre, the two sides of bottom case are vertically installed with transfusion pole outside the intelligent control center, if the transfusion pole bottom there are
Dry spray head.
Further, the wind-force pressure exerting arrangement includes rotor driver, and the rotor driver is fixed on rotor branch vertically
On frame, rotor driver bottom output end is equipped with rotor.
Further, assembling activity bolt on the cockpit side wall, the activity bolt and supporting leg overturning cooperate.
Further, flight support main body back is equipped with water tank, and the output end and transfusion pole of the water tank input
End connection.
Further, the flight support bottom part body is mounted with center feed liquid cabin, center feed liquid cabin stem it is defeated
Exit port is connect with seedling distributing device, and the two groups of wheel carriers and flight support bottom part body of center feed liquid cabin two sides distribution are fixed to be connected
It connects, the wheel carrier and thrust wheel limit cooperate.
Further, the flight support main body neck front and rear sides pass after being respectively fitted with machine front sensor assembly and machine
Sensor assembly.
After adopting the above structure, compared with prior art, the present invention is a kind of landing-type fog machine, using single wheel single track
Motion mode, solve the occupied area for reducing value preserving machine, while also reducing value preserving machine own wt, reduce ridge
Destructive rate.Built-in rotor balance system solves the technical issues of fuselage inclination.Brief body construction is more suitable for nobody and drives
It sails.
Detailed description of the invention
The present invention will be further described in detail below with reference to the accompanying drawings and specific embodiments.
Fig. 1 is the main view of the dynamic mixed intelligent fog machine of the more rotor fuels of the present invention.
Fig. 2 is the left view of the dynamic mixed intelligent fog machine of the more rotor fuels of the present invention.
In figure: 1 being rotor bracket, 2 be sensor unit after machine, 3 be power organ case, 4 be water tank, 5 be split type medicine
Case, 6 be spray head, 7 be thrust wheel, 8 be machine front sensor assembly, 9 be cockpit, 10 be seedling distributing device, 11 be rotor, 12 centered on
Feed liquid cabin, 13 be rotor driver, 14 be intelligent control center, 15 be supporting leg, 16 be flight support main body, 17 be infusion
Bar.
Specific embodiment
As depicted in figs. 1 and 2, the dynamic mixed intelligent fog machine of the more rotor fuels of a kind of single-track, including flight support main body；It is described
It is equipped with wind-force pressure exerting arrangement on 16 top rotor bracket 1 of flight support main body, equipped with cockpit 9 in the rotor bracket 1,
It is equipped with split type medicine-chest 5 at left and right sides of the cockpit 9, is mounted with intelligent control center 14, institute in 9 pedestal of cockpit
The two sides for stating 14 outside bottom case of intelligent control center are vertically installed with transfusion pole 17, and there are several spray heads for 17 bottom of transfusion pole
6.Wherein, start fog machine, split type medicine-chest 5 transports medical fluid by intelligent control center 14 defeated to being subject in transfusion pole 17
Out, during output, the separation pressure exerting arrangement on rotor bracket 1 will generate the wind pressure of strength, and script is sprayed route sheet
One atomization medical fluid further expands diffusion area.
As shown in Fig. 2, the wind-force pressure exerting arrangement includes rotor driver 13, the rotor driver 13 is fixed on vertically
On rotor bracket 1, the 13 bottom output end of rotor driver is equipped with rotor 11.Wherein, wind-force pressure exerting arrangement by
Rotor driver 13 is installed to drive rotor 11 to rotate on rotor bracket 1, so that downward wind pressure is generated, final expansion atomization
The range of scatter of medical fluid.
As shown in Fig. 2, assembling activity bolt on 9 side wall of cockpit, the activity bolt and the overturning of supporting leg 15 cooperate.Its
In, since the fog machine of single-wheel is not easy steadily to stand in the state of stopping operating, assembled on 9 side wall of cockpit
Movable bolt.Cooperated using movable bolt and the overturning of supporting leg 15, to keep organism balance.
As shown in Figure 1,16 back of flight support main body is equipped with water tank 4, the output end and transfusion pole of the water tank 4
The connection of 17 input terminals.Wherein, the water tank 4 of 16 back of flight support main body installation is connect with 17 input terminal of transfusion pole.It substantially reduces
Water tank 4 is in the intracorporal occupied area of machine.
As shown in Figure 1,16 bottom loaded of flight support main body has center feed liquid cabin 12, center feed liquid cabin 12 is first
The output port in portion is connect with seedling distributing device 10, the two groups of wheel carriers and flight support main body 16 of the distribution of 12 two sides of center feed liquid cabin
Bottom is fixedly connected, and the wheel carrier and the limit of thrust wheel 7 cooperate.
As shown in Figure 1, the 16 neck front and rear sides of flight support main body are respectively fitted with machine front sensor assembly 8 and machine
Sensor unit 2 afterwards.Wherein, due to the fog machine be biased to it is unmanned, in order to enhance the autonomous operating capability of body
And balanced capacity, machine front sensor assembly 8 and machine are respectively fitted in the 16 neck front and rear sides of flight support main body
Sensor unit 2 afterwards.
A set of more rotor systems, robot base setting front and back two wheels of single-column type are set at the top of machine, i.e. single-track is transported
Dynamic system.The all components such as device spray, broadcast application on wheel carrier, control system are the driving of full Intelligent unattended and flight control system.It is more
Rotor system is mainly responsible for the balance of mechanical movement, and wheel group mainly undertakes total weight and travel speed and the direction of machine,
Control system and operating system respectively complete the intelligence of oneself.
When machine is static, the supporting leg of two sides is put down, and is propped up fuselage and is first started more rotor balance systems when machine is run,
Its Rotor thrust will keep the left-right balance of car body, then supporting leg is packed up, and wheel band movement machine moves forward or back.Two wheels
One of them be it is height-adjustable, under the control of obliquity sensor and intelligence system, keep car body anterior-posterior balance.
Other operations repeat no more.
1, due to single-track, so it is suitble to the field of any line-spacing, it is without any requirement to line-spacing and shape；
2, since single line fulcrum rotor balances, so equipment can remain left-right balance regardless of how uneven field is；
3, due to only former and later two wheels, so can very simply by a certain wheel design be the adjustable mode of height, in this way before
After balance and can all accomplish to automatically control；
4, due to being single-track, machine can go to the turning of field edge, guarantee not hurt plant seedlings when turning u-turn；
5, due to there is uniline wheel supporting, so the biggish generator of installation weight and big medicine-chest and a variety of auxiliary is supported to set
It is standby；
6, due to overcoming the problem of car body is tilted to two sides, so spray boom can be accomplished to grow very much, it is greatly improved spray drug operation
Efficiency；
7, due to the disturbance of rotor wind-force, make the medicine mist sprayed attachment more it is even more comprehensively；
8, due to there is enough load-carrying abilities, so the configurable comparable widespread device of capacity；
9, due to being very suitable to unmanned control with rotor balance system and uniline wheel；
10, due to the upper pulling force of brief body construction and more rotors, be greatly lowered main screw lift, be more suitable paddy field work
Industry；
11, since more rotor systems are only responsible for balance, very big promotion power output is not undertaken, so power generation requirement is than pure oil electricity
It flies much lower, so that the volume and weight of generator is also greatly lowered；
12, under the premise of the performance of the design of unique structure and brilliance possesses, under year-on-year cost is at a fairly low, therefore this product has
There is very high cost performance.
Claims (6)
1. a kind of dynamic mixed intelligent fog machine of more rotor fuels of single-track, including flight support main body；It is characterized in that: the flight support
It is equipped with wind-force pressure exerting arrangement at the top of main body (16) on rotor bracket (1), equipped with cockpit (9) in the rotor bracket (1),
It is equipped with split type medicine-chest (5) at left and right sides of the cockpit (9), is mounted in intelligent control in cockpit (9) pedestal
The two sides of the heart (14), the external bottom case of the intelligent control center (14) are vertically installed with transfusion pole (17), the transfusion pole (17)
There are several spray heads (6) for bottom.
2. the dynamic mixed intelligent fog machine of the more rotor fuels of single-track according to claim 1, it is characterized in that: the wind-force pressing machine
Structure includes rotor driver (13), and the rotor driver (13) is fixed on rotor bracket (1) vertically, the rotor driver
(13) bottom output end is equipped with rotor (11).
3. the dynamic mixed intelligent fog machine of the more rotor fuels of single-track according to claim 1, it is characterized in that: the cockpit (9)
Assembling activity bolt on side wall, the activity bolt and supporting leg (15) overturning cooperate.
4. the dynamic mixed intelligent fog machine of the more rotor fuels of single-track according to claim 1, it is characterized in that: the flight support master
Body (16) back is equipped with water tank (4), and the output end of the water tank (4) is connect with transfusion pole (17) input terminal.
5. the dynamic mixed intelligent fog machine of the more rotor fuels of single-track according to claim 1, it is characterized in that: the flight support master
Body (16) bottom loaded has center feed liquid cabin (12), and the output port of center feed liquid cabin (12) stem and seedling distributing device (10) are even
It connects, two groups of wheel carriers of center feed liquid cabin (12) two sides distribution are fixedly connected with flight support main body (16) bottom, the wheel
Frame and thrust wheel (7) limit cooperate.
6. the dynamic mixed intelligent fog machine of the more rotor fuels of single-track according to claim 1, it is characterized in that: the flight support master
Body (16) neck front and rear sides are respectively fitted with sensor unit (2) after machine front sensor assembly (8) and machine.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811205221.7A CN109315378A (en) | 2018-10-16 | 2018-10-16 | The dynamic mixed intelligent fog machine of the more rotor fuels of single-track |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811205221.7A CN109315378A (en) | 2018-10-16 | 2018-10-16 | The dynamic mixed intelligent fog machine of the more rotor fuels of single-track |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109315378A true CN109315378A (en) | 2019-02-12 |
Family
ID=65262531
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811205221.7A Pending CN109315378A (en) | 2018-10-16 | 2018-10-16 | The dynamic mixed intelligent fog machine of the more rotor fuels of single-track |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109315378A (en) |
Citations (16)
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|---|---|---|---|---|
| GB755965A (en) * | 1953-11-19 | 1956-08-29 | Fairey Aviat Co Ltd | Improvements relating to rotary wing aircraft |
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-
2018
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| CN103661946A (en) * | 2013-12-13 | 2014-03-26 | 江苏大学 | Flow diversion anti-drifting devices for rotary-wing unmanned plane mist spraying |
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