CN202722341U - Telecontrolled aircraft powder spayer - Google Patents
Telecontrolled aircraft powder spayer Download PDFInfo
- Publication number
- CN202722341U CN202722341U CN 201220291304 CN201220291304U CN202722341U CN 202722341 U CN202722341 U CN 202722341U CN 201220291304 CN201220291304 CN 201220291304 CN 201220291304 U CN201220291304 U CN 201220291304U CN 202722341 U CN202722341 U CN 202722341U
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- powder
- telecontrolled aircraft
- powder tank
- spayer
- aircraft
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Abstract
The utility model discloses a telecontrolled aircraft powder spayer which is mounted at the bottom of a telecontrolled aircraft, wherein the telecontrolled aircraft is provided with a central controller, the telecontrolled aircraft powder spayer comprises an elastic pipe, one end of the elastic pipe is closed, and the other end of the elastic pipe is connected with a spay nozzle through a solenoid valve. The spay nozzle is inserted into a powder tank and extends to the bottom of the powder tank; a powder outlet is arranged on a position, on the bottom surface of the powder tank, located under the spay nozzle; a powder spraying pipeline is located under the powder tank and communicated with the interior of the powder tank through the powder outlet. According to the telecontrolled aircraft powder spayer, an air pump in the prior art and a storage battery device which provides electricity for the air pump are saved, so that the weight of the powder spayer is greatly reduced, and therefore the weight of powder carried by the powder spayer can be accordingly added. The telecontrolled aircraft powder spayer is simple in structure, convenient to manufacture and operate, and capable of effectively improving work efficiency.
Description
Technical field
The utility model relates to the application of Miniature remote control unmanned aerial vehicle, especially a kind of telecontrolled aircraft dusting device.
Background technology
The miniature self-service telecontrolled aircraft is the aircraft of controlling by wireless remote controller, is provided with central controller on the aircraft, can be divided into fixed-wing telecontrolled aircraft and RC Goblin according to the kind of its wing.The miniature self-service telecontrolled aircraft has a volume little, cheap for large-scale manned aircraft, maneuverability, and the easily characteristics of rising and falling are widely used in agricultural, fire-fighting and the field of taking photo by plane.
In agricultural, often can spray the operation of the pulverulent solids such as power pesticide or pollen, use at present manual type dusting operation workload large, and inefficiency.Adopt the large aircraft operation of dusting to be only applicable to the bulk farmland, be not suitable for the fritter field.But when dusting operation with the miniature self-service telecontrolled aircraft, can solve inefficiency in the artificial By Dusting process and the at present large aircraft operation of dusting is unsuitable for the problem of haggard, yet dusting device of the prior art, must cooperate air pump and use for air pump provides the accumulator plant of electric power, and the loading capacity of SUAV own is limited, the weight that has increased air pump namely means the weight that reduces corresponding powder, the minimizing of the powder amount of carrying so that the area that at every turn dusts reduce, thereby reduced operating efficiency.
The utility model content
The technical problems to be solved in the utility model provides and a kind ofly need not to use air pump to pressurize, and can finish equally the telecontrolled aircraft dusting device of the operation of dusting.
For addressing the above problem, a kind of telecontrolled aircraft dusting device of the present utility model, be installed in the bottom of telecontrolled aircraft, be provided with central controller on the telecontrolled aircraft, described telecontrolled aircraft dusting device comprises elastic tubes, the end sealing of described elastic tubes, and its other end links to each other with nozzle by magnetic valve, described nozzle inserts in the powder tank and extends to the powder pot bottom, offers flour opening on the powder tank bottom surface and the position that is positioned at below the nozzle; One pipeline that dusts is positioned at powder tank below, and by flour opening and powder tank internal communication.
The bottom of described powder tank is the reverse taper shape.
Described elastic tubes helical form is wrapped on the outer wall of powder tank.
The described pipeline that dusts is horizontally installed on the bottom of telecontrolled aircraft, offers groove on its lower end tube wall.
Described elastic tubes is silicone tube.
Described elastic tubes is emulsion tube.
Adopt the telecontrolled aircraft dusting device of the utility model structure, gas injection in elastic tubes at first, elastic tubes is expanded in the scope that its elasticity allows, telecontrolled aircraft flies to waiting the sky, zone of dusting during use, magnetic valve is opened in remote control, make gas under the tension force effect of elastic tubes self, be squeezed into the powder tank, thus with the powder in the powder tank in flour opening place ejection and enter in the pipeline that dusts, and then outwards spray by the groove on the pipeline that dusts.Telecontrolled aircraft dusting device of the present utility model, compared with prior art has following beneficial effect: the accumulator plant of having saved air pump of the prior art and electric power being provided for air pump, greatly alleviate the weight of dusting device, thereby can correspondingly increase the weight of its powder that carries; The utility model is simple in structure, the convenient making, and convenient operation can Effective Raise production efficiency.
Description of drawings
Fig. 1 is the utility model telecontrolled aircraft dusting device mounting structure schematic diagram.
Fig. 2 is the perspective view of the utility model telecontrolled aircraft dusting device.
Fig. 3 is the front view of the utility model telecontrolled aircraft dusting device.
Fig. 4 is that the A-A of Fig. 3 is to cutaway view.
Embodiment
In order to make those skilled in the art person understand better technical solutions of the utility model, the utility model is described in further detail below in conjunction with drawings and embodiments.
As shown in Figures 1 to 4, a kind of telecontrolled aircraft dusting device 2 of the present utility model, be installed in the bottom of telecontrolled aircraft 1, comprise elastic tubes 201, the one end sealing of described elastic tubes 201, its other end links to each other with nozzle 203 by magnetic valve 202, and it is interior and extend to powder tank 204 bottoms that described nozzle 203 inserts powder tanks 204, offers flour opening 205 on powder tank 204 bottom surfaces and the position that is positioned at below the nozzle 203; One pipeline 206 that dusts is positioned at powder tank 204 belows, and by being connected to the tube connector 207 and powder tank 204 internal communication on the flour opening 205.
The described pipeline 206 that dusts is horizontally installed on the bottom of telecontrolled aircraft 1, offers groove 208 on its lower end tube wall.
Described magnetic valve 202 links to each other with central controller (not shown) on the telecontrolled aircraft 1, and operating personnel can control in the face of telecontrolled aircraft 1 on ground, and can control magnetic valve 202 and open or close.
At first at elastic tubes 201 interior gas injections, elastic tubes 201 is expanded in the scope that its elasticity allows, telecontrolled aircraft flies to waiting the sky, zone of dusting during use, magnetic valve 202 is opened in remote control, make gas under the tension force effect of elastic tubes 201 self, be squeezed into powder tank 204, thereby the powder in the powder tank 204 in the ejection of flour opening 205 places and enter in the pipeline 206 that dusts, and then are outwards sprayed by the groove 208 on the pipeline 206 that dusts.
Because nozzle 203 is positioned at the top of flour opening 205, air-flow can only directly act on the position of the top of flour opening 205 after by nozzle 203, pile up in the bottom of powder tank 204 in order to prevent powder, the bottom of described powder tank 204 can be set to the back taper bodily form, when air-flow blows out the powder of close flour opening 205 positions, the powder that is positioned at other positions can be along the landing of reverse taper inwall to flour opening 205 places, so not again the bottom of powder tank 204 pile up.
In order to take full advantage of the space of telecontrolled aircraft 1 bottom, can say that elastic tubes 201 is wrapped on the outer wall of powder tank 204 with helical form.
Described elastic tubes 201 is emulsion tube.Emulsion tube is the different pipe of thickness that the latex material is made, and is mainly used in the fields such as hospital, instrument factory, power plant, scientific experiment chamber, more relates to the public places of entertainment such as bungee jumping, trampoline.The characteristic of emulsion tube is that elastic force is good, and general weight range can be at self 6-9 times, screen resilience 100%.In the utility model, gas injection in emulsion tube, emulsion tube is expanded in the scope that its elasticity allows, telecontrolled aircraft flies to the zone of dusting overhead during use, magnetic valve is opened in remote control, make gas under the tension force effect of elastic tubes self, be squeezed into the powder tank, thereby the powder in the powder tank is sprayed at the nozzle place.By the resilience tension force that the emulsion tube after expanding himself has the gas of its inside is exerted pressure, need not additionally to add supercharging device, and then alleviated the overall weight of dusting device.
Certainly, described elastic tubes can also be silicone tube.Silicone tube is to be processed by silicon rubber, silicon rubber is a kind of novel macromolecular material, and fabulous high temperature resistant and resistance to low temperature is arranged, and good physiological stability is arranged, and can stand repeated multiple times harshness and conditions for sterilization, have splendid resilience and permanent deformation little.
The above only is preferred embodiment of the present invention; should be pointed out that for those skilled in the art, under the prerequisite that does not break away from the principle of the invention; can also make some improvements and modifications, these improvements and modifications also should be considered as protection scope of the present invention.
Claims (6)
1. telecontrolled aircraft dusting device, be installed in the bottom of telecontrolled aircraft, be provided with central controller on the telecontrolled aircraft, it is characterized in that: described telecontrolled aircraft dusting device comprises elastic tubes, the one end sealing of described elastic tubes, its other end links to each other with nozzle by magnetic valve, and described nozzle inserts in the powder tank and extends to the powder pot bottom, offers flour opening on the powder tank bottom surface and the position that is positioned at below the nozzle; One pipeline that dusts is positioned at powder tank below, and by flour opening and powder tank internal communication.
2. telecontrolled aircraft dusting device as claimed in claim 1, it is characterized in that: the bottom of described powder tank is the reverse taper shape.
3. telecontrolled aircraft dusting device as claimed in claim 2, it is characterized in that: described elastic tubes helical form is wrapped on the outer wall of powder tank.
4. telecontrolled aircraft dusting device as claimed in claim 3, it is characterized in that: the described pipeline that dusts is horizontally installed on the bottom of telecontrolled aircraft, offers groove on its lower end tube wall.
5. such as each described telecontrolled aircraft dusting device of claim 1 to 4, it is characterized in that: described elastic tubes is silicone tube.
6. such as each described telecontrolled aircraft dusting device of claim 1 to 4, it is characterized in that: described elastic tubes is emulsion tube.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220291304 CN202722341U (en) | 2012-06-20 | 2012-06-20 | Telecontrolled aircraft powder spayer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220291304 CN202722341U (en) | 2012-06-20 | 2012-06-20 | Telecontrolled aircraft powder spayer |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202722341U true CN202722341U (en) | 2013-02-13 |
Family
ID=47648108
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220291304 Expired - Lifetime CN202722341U (en) | 2012-06-20 | 2012-06-20 | Telecontrolled aircraft powder spayer |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202722341U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104957033A (en) * | 2015-07-13 | 2015-10-07 | 绍兴文理学院 | Chinese torreya pollination unmanned plane and use method of Chinese torreya pollination unmanned plane |
| CN105966621A (en) * | 2016-06-15 | 2016-09-28 | 遵义市林业科学研究所 | Dust spraying machine for unmanned aerial vehicle |
-
2012
- 2012-06-20 CN CN 201220291304 patent/CN202722341U/en not_active Expired - Lifetime
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104957033A (en) * | 2015-07-13 | 2015-10-07 | 绍兴文理学院 | Chinese torreya pollination unmanned plane and use method of Chinese torreya pollination unmanned plane |
| CN104957033B (en) * | 2015-07-13 | 2017-04-19 | 绍兴文理学院 | Chinese torreya pollination unmanned plane and use method of Chinese torreya pollination unmanned plane |
| CN105966621A (en) * | 2016-06-15 | 2016-09-28 | 遵义市林业科学研究所 | Dust spraying machine for unmanned aerial vehicle |
| CN105966621B (en) * | 2016-06-15 | 2019-01-15 | 遵义市林业科学研究所 | A kind of unmanned plane powder blower |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term | ||
| CX01 | Expiry of patent term |
Granted publication date: 20130213 |