CN206590127U - A kind of unmanned fog machine spray equipment - Google Patents
A kind of unmanned fog machine spray equipment Download PDFInfo
- Publication number
- CN206590127U CN206590127U CN201720264090.4U CN201720264090U CN206590127U CN 206590127 U CN206590127 U CN 206590127U CN 201720264090 U CN201720264090 U CN 201720264090U CN 206590127 U CN206590127 U CN 206590127U
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- China
- Prior art keywords
- water tank
- flexible pipe
- spray equipment
- fog machine
- water
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- 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.)
- Expired - Fee Related
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Abstract
A kind of unmanned fog machine spray equipment; water tank including being evenly distributed on each position of fuselage, each water tank is connected by flexible pipe with water pump, and water pump is connected to each nozzle by flexible pipe; after pump working; by water tank inner liquid medicine suction hose, into nozzle, pass through the atomising device in nozzle; form medicine mist; prop-blast stirs medicine mist, it is further evenly distributed, trickles down on the crops of lower section.Complete after a spraying operation, return to place of setting out, change battery, decoction is filled into medicine-chest, the second subjob can be carried out；The bottom of each water tank of the utility model is connected by flexible pipe, water tank is evenly distributed on each position of fuselage, water in original water tank is distributed evenly in each sub- water tank, machine gravity knots modification can be obviously reduced when fuselage rocks, it is connected between each sub- water tank using linker, to ensure that each sub- water tank Chinese medicine water level is highly consistent；With practicality it is reliable, compatible good the characteristics of.
Description
Technical field
The utility model is related to a kind of agricultural plant protection machinery, more particularly to a kind of unmanned fog machine spray equipment.
Background technology
Domestic fog machine at present is also in the stage of development, and existing product still suffers from many weak points.Such as, due to electricity
The limitation of pond electricity and body physical burden, unmanned plane cruising time is shorter, and single drugloading rate is less；Due to its structure design not
Rationally, rocking for liquid medicine causes unmanned plane during flying unstable in medicine-chest, and liquid medicine may be sprayed onto on circuit board during spray,
So as to cause line fault.The shortcomings of wherein battery durable is short needs the breakthrough of science and technology to improve, but decoction rocks
It can be reduced or eliminate using cleverly Design of Mechanical Structure etc. defect.
The content of the invention
In order to overcome the above-mentioned deficiencies of the prior art, the purpose of this utility model is the provision of a kind of unmanned fog machine spray
Shower device, can farthest reduce influence of the medicine-chest to state of flight in flight course so that rock can for liquid medicine in medicine-chest
To be effectively suppressed；Medicine-chest capacity is big, and distribution of weight is uniform, also allows for the exploitation that fog machine flies control, with it is practical it is reliable,
The characteristics of compatibility is good.
To achieve these goals, the technical solution adopted in the utility model is：
A kind of unmanned fog machine spray equipment, including it is evenly distributed on the water tank 1 of each position of unmanned aerial vehicle body, each water
Case 1 is connected by flexible pipe 2 with water pump 3, and water pump 3 is connected to each nozzle 4 by flexible pipe 2, and the bottom of each water tank 1 passes through soft
Pipe 2 is connected.
Described nozzle 4 is plastic products, and inside is stainless steel making.
Described flexible pipe 2 is PVC hose, and inner wall thickness is 1.5mm.
Described water pump 3 is using brushless electric machine as power, and motor side is sealed using aluminum hull.
Described water tank 1 makes for light plastic, is shaped as back taper design.
Liquid level detection device is provided with any one described water tank 1.
Described nozzle 4 is arranged on close to the position below propeller.
The utility model has advantages below：
(1) water tank uses Distributed Design, and liquid medicine weight average is distributed on each propeller.Plant protection water tank side on the market
Case general choice list water tank, this can cause drugloading rate in single water tank too high, once unmanned plane speed changes, or direction changes,
Liquid medicine can be rocked acutely in water tank, cause fuselage to rock, and even fuselage diversity concussion when serious, finally winged control can not correct winged
Row device posture, causes aircraft bombing.In view of this point, large water tank is split into several sub- water tanks by this programme, and is evenly distributed on fuselage
Each position, the water in large water tank is distributed evenly in each sub- water tank, and machine gravity knots modification can be obvious when fuselage rocks
Reduce.When i.e. aircraft momentum changes, disperse the impulsive force of the liquid medicine in water tank, fuselage can be effectively reduced and rocked.Water tank is removable
Unload, take off again without filling decoction again, change bottle and fly.
2) each sub- water tank is designed using back taper, is cylindrical structural above water tank, and lower section is gradually drawn in, and radius is slow
It is slow to reduce, it is punctured into taper.Liquid medicine rocks the influence to aspect when such a design can reduce flight.If not using cone bottom
Design, when liquid medicine surplus is less than half, can produce stronger impact to water tank wall when liquid medicine is rocked.
3) nozzle is arranged on close to the position below propeller, is sprayed after medicine mist, can be stirred air-flow by propeller, be made medicine
Mist is uniformly distributed, when liquid medicine falls crops downwards, crops drug effect fruit more preferable.
4) it is connected between each sub- water tank using linker, to ensure that each sub- water tank Chinese medicine water level highly keeps one
Cause.If not increasing linker, if each sub- water tank goes out dose difference, it is varied in weight, aircraft center of gravity will be caused to offset, no
Beneficial to aircraft smooth flight.
5) remove the trouble of cleaning medicine-chest from, when changing different decoctions, only need to change sub- water tank, flusher is cleaned with clear water
；Modularized design is used simultaneously, such as crash injury, changing correlation module can reuse, and continuous operation ability is big
Width is lifted.
Brief description of the drawings
Fig. 1 is the utility model structural representation.
Fig. 2 is quadrotor schematic diagram.
Embodiment
Structural principle of the present utility model and operation principle are described in further detail below in conjunction with the accompanying drawings.
Referring to Fig. 1, Fig. 2, a kind of unmanned fog machine spray equipment by taking quadrotor as an example, including is evenly distributed on
The water tank 1 of 4 positions of quadrotor fuselage, four water tanks 1 are placed close to each propeller, make weight be evenly distributed on nobody
Machine corner, square distribution.4 water tanks 1 are connected by flexible pipe 2 with water pump 3, and water pump 3 is connected to each by flexible pipe 2 and sprayed
Mouth 4, the bottom of each water tank 1 is connected by flexible pipe 2, by intercommunicating device so that liquid level keeps phase same level in four medicine bottles
State, liquid level detection device at a water tank interface, inserts medicine-chest wherein when using, for real-time level monitoring.
Flexible pipe 2 and water tank 1, the interface of water pump 3 are handled using sealant sealing, prevent decoction from spilling.The delivery port of nozzle 4
Downwards, the possibility that liquid medicine penetrates into motor is reduced as far as possible, otherwise for a long time inside meeting corrosion electrical motor.Nozzle mounting position, which is tried one's best, to be leaned on
Nearly motor cabinet, can both reduce medicine mist float frame central control board in, propeller wind-force can be effectively utilized again, makes medicine
Mist is homogenized.Water pump 3 is made using DC brushless motor, can be powered using 12V-16V, is substantially with multi-rotor aerocraft motor
Similarly configure, can be powered using battery of the same type, same model electricity transfer drive is moved.
Described nozzle 4 is plastic products, and inside is stainless steel making, and service life is can ensure that from stainless steel
It is long, reach 3 times of brass material life-span.Injection diameter is 1.0mm, and spray angle is maximum up to 80 degree, and adjustment spray angle can
Regulating liquid medicine fogging degree.
Described flexible pipe 2 is PVC hose, and elasticity is good, and resistance corrosion, and inner wall thickness is 1.5mm.
Described water pump 3 is using brushless electric machine as power, and motor side is sealed using aluminum hull, dustproof and waterproof antirust, and is dissipated
Thermal effect is good, lighter in weight.
Described water tank 1 is that light plastic makes, and is shaped as back taper design, is effectively reduced liquid medicine in medicine-chest and rocks pair
The influence of unmanned plane stability, and when liquid medicine is gradually used up, the back taper design of bottom can also make the liquid medicine rocked to nobody
The influence of machine center of gravity is minimum.
Described nozzle 4 is arranged on close to the position below propeller, is sprayed after medicine mist, can stir gas by propeller
Stream, is uniformly distributed medicine mist,
Operation principle of the present utility model is：
Water tank 1 is evenly distributed on each position of fuselage, and the water in original water tank is distributed evenly in each sub- water tank 1,
Machine gravity knots modification can be obviously reduced when fuselage rocks.It is connected between each sub- water tank 1 using linker, to ensure each son
Water tank Chinese medicine water level is highly consistent.After water pump 3 works, the inner liquid medicine suction hose 2 of water tank 1, into nozzle 4, leads to
The atomising device crossed in nozzle 4, forms medicine mist.Prop-blast stirs medicine mist, it is further evenly distributed, trickles down in lower section
On crops.Complete after a spraying operation, return to place of setting out, change battery, decoction is filled into medicine-chest, can carry out second
Operation.
Claims (7)
1. a kind of unmanned fog machine spray equipment, it is characterised in that the water including being evenly distributed on each position of unmanned aerial vehicle body
Case (1), each water tank (1) is connected by flexible pipe (2) with water pump (3), and water pump (3) is connected to each nozzle by flexible pipe (2)
(4), the bottom of each water tank (1) is connected by flexible pipe (2).
2. a kind of unmanned fog machine spray equipment according to claim 1, it is characterised in that described nozzle (4) is modeling
Material products, inside is stainless steel making.
3. a kind of unmanned fog machine spray equipment according to claim 1, it is characterised in that described flexible pipe (2) is PVC
Flexible pipe, inner wall thickness is 1.5mm.
4. a kind of unmanned fog machine spray equipment according to claim 1, it is characterised in that described water pump (3) is used
Brushless electric machine is sealed as power, motor side using aluminum hull.
5. a kind of unmanned fog machine spray equipment according to claim 1, it is characterised in that described water tank (1) is light
Matter plastic production, is shaped as back taper design.
6. a kind of unmanned fog machine spray equipment according to claim 1, it is characterised in that any one described water tank
(1) liquid level detection device is provided with.
7. a kind of unmanned fog machine spray equipment according to claim 1, it is characterised in that described nozzle (4) is installed
Close to the position below propeller.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720264090.4U CN206590127U (en) | 2017-03-17 | 2017-03-17 | A kind of unmanned fog machine spray equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720264090.4U CN206590127U (en) | 2017-03-17 | 2017-03-17 | A kind of unmanned fog machine spray equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206590127U true CN206590127U (en) | 2017-10-27 |
Family
ID=60123455
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720264090.4U Expired - Fee Related CN206590127U (en) | 2017-03-17 | 2017-03-17 | A kind of unmanned fog machine spray equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206590127U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108522467A (en) * | 2018-03-07 | 2018-09-14 | 芜湖翼讯飞行智能装备有限公司 | A kind of pesticide spraying unmanned plane |
| CN108739262A (en) * | 2018-06-15 | 2018-11-06 | 胡立波 | A kind of unmanned plane flower-watering device |
-
2017
- 2017-03-17 CN CN201720264090.4U patent/CN206590127U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108522467A (en) * | 2018-03-07 | 2018-09-14 | 芜湖翼讯飞行智能装备有限公司 | A kind of pesticide spraying unmanned plane |
| CN108739262A (en) * | 2018-06-15 | 2018-11-06 | 胡立波 | A kind of unmanned plane flower-watering device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20171027 Termination date: 20210317 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |