CN209581865U - One kind having heat sinking function plant protection drone - Google Patents
One kind having heat sinking function plant protection drone Download PDFInfo
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- CN209581865U CN209581865U CN201920128850.8U CN201920128850U CN209581865U CN 209581865 U CN209581865 U CN 209581865U CN 201920128850 U CN201920128850 U CN 201920128850U CN 209581865 U CN209581865 U CN 209581865U
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Abstract
There is heat sinking function plant protection drone the utility model relates to a kind of.The technical solution adopted is that: including drone body, lithium battery, fly control module, power plant module, lithium battery, winged control module, power plant module.On the one hand the utility model passes through increase cooling tube and radiator cools down the especially power plant module of device in drone body, avoids unmanned plane interior arrangement since overheat reduces unmanned plane, damages unmanned plane, increases maintenance cost;On the other hand by increasing hygrosensor and cooling piece, the liquid looped back is cooled down, the service life of unmanned plane is increased;Have the advantages that structure is simple, manipulation is convenient, save manpower, avoid loss, is high-efficient, working effect is obvious etc..
Description
Technical field
The utility model belongs to air vehicle technique field, is related to a kind of with heat sinking function plant protection drone.
Background technique
Plant protection drone is to be carried out for the UAV of agriculture and forestry plant protection operation by navigating or being remotely controlled
Fly control, realizes the work such as the sprinkling, sowing, fertilising of drug.But the working environment of plant protection drone be often great work intensity,
Need flying for long time, matter-loading amount big, on the one hand, unmanned plane own vol is smaller, so that unmanned plane internal heat dissipating effect is very
Difference;On the other hand, power plant module is easy fever during long-play, so that power plant module breaks down, is not able to satisfy
Use demand of the people to unmanned plane.
Utility model content
In view of the problems of in the prior art, the utility model discloses one kind have heat sinking function plant protection nobody
Machine, the technical solution adopted is that, including drone body, lithium battery, winged control module, power plant module, drone body inside is
Hollow structure, lithium battery, winged control module, power plant module are located inside drone body, lithium battery and winged control module, power plant module
Connection, which is characterized in that further include annular partition, cooling tube, radiator, wherein the annular partition is located at drone body
Inside, the cooling tube are located among drone body inner wall and annular partition, and the radiator is located in drone body
Rear portion.
As a kind of preferred embodiment of the use of the new type, the radiator includes outlet tube, inlet tube, baffle, temperature
Detector, pump, check valve, cooling piece, pipeline, wherein radiator is divide into upper part and lower part by the baffle, the cooling piece
Positioned at baffle upper surface, the hygrosensor is located at radiator internal upper part left side wall, and the pipeline is connected on radiator
Lower two parts install check valve on the pipeline, and the outlet tube is located at radiator upper half rear wall, and the inlet tube is located at
Radiator lower half rear wall, the cooling tube upper port are connect with outlet tube, and the cooling infratubal port is connect with inlet tube,
The pump is connect with inlet tube, and the pump, cooling piece are connect with control module is flown, and the hygrosensor is connect with control module is flown.
As a kind of preferred embodiment of the use of the new type, the cooling tube is helical form, and material is conduction copper.
The utility model has the beneficial effects that on the one hand the utility model passes through increases cooling tube and radiator, to nobody
Machine this vivo devices especially power plant module, cools down, and avoids unmanned plane interior arrangement since overheat reduces unmanned plane,
Unmanned plane is damaged, maintenance cost is increased;On the other hand by increasing hygrosensor and cooling piece, to the liquid looped back into
Row cooling, increases the service life of unmanned plane;It is simple with structure, manipulation is convenient, save manpower, avoid loss, is high-efficient,
The advantage that working effect obviously waits.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model;
Fig. 2 is schematic cross-sectional view on the right side of the utility model;
Fig. 3 is schematic cross-sectional view on rear side of the utility model;
In figure: 1- drone body, 2- annular partition, 3- cooling tube, 4- lithium battery, 5- fly control module, 6- power plant module,
7- radiator, 701- outlet tube, 702- inlet tube, 703- baffle, 704- hygrosensor, 705- pump, 706- check valve,
707- cooling piece, 708- pipeline.
Specific embodiment
Embodiment 1
As shown in Figure 1, Figure 2, Figure 3 shows, including drone body 1, lithium battery 4, fly control module 5, power plant module 6, unmanned plane
Be hollow structure inside ontology 1, lithium battery 4 flies control module 5, power plant module 6 and is located inside drone body 1, lithium battery 4 and
Fly control module 5, power plant module 6 connects, which is characterized in that further include annular partition 2, cooling tube 3, radiator 7, wherein described
Annular partition 2 is located inside drone body 1, and the cooling tube 3 is located among 1 inner wall of drone body and annular partition 2, institute
It states radiator 7 and is located at rear portion in drone body 1;The radiator 7 includes outlet tube 701, inlet tube 702, baffle
703, hygrosensor 704, pump 705, check valve 706, cooling piece 707, pipeline 708, wherein the baffle 703 is by radiator
7 are divide into upper part and lower part, and the cooling piece 707 is located at 703 upper surface of baffle, and the hygrosensor 704 is located at radiator 7
Internal upper part left side wall, the pipeline 708 are connected to about 7 two parts of radiator, install check valve 706, institute on the pipeline 708
It states outlet tube 701 and is located at 7 upper half rear wall of radiator, the inlet tube 702 is located at 7 lower half rear wall of radiator, described
3 upper port of cooling tube is connect with outlet tube 701, and 3 lower port of cooling tube is connect with inlet tube 702, the pump 705 and feed liquor
Pipe 702 connects, and the pump 705, cooling piece 707 are connect with control module 5 is flown, and the hygrosensor 704 connects with control module 5 is flown
It connects;The cooling tube 3 is helical form, and material is conduction copper.
Working principle of the utility model is: peasant household's manipulation unmanned plane or setting unmanned plane course line carry out the spray of high-altitude drug
It spills, apply fertilizer, in unmanned plane operation process, fly control module 5 and control the opening of check valve 706, coolant liquid enters 7 bottom of radiator
Portion is entered inside cooling tube 3 by pump 705, carries out radiating and cooling to 1 interior arrangement of drone body especially power plant module 6
Processing;Hygrosensor 704 carries out temperature detection to the coolant liquid that 7 upper half of radiator is placed simultaneously, works as hygrosensor
704 to setting value when, fly control module 5 and control cooling piece 707 to carry out it refrigeration processing, coolant liquid is followed by cooling tube 3
Ring cooling.
The electronic component that the utility model uses can be bought easily on the market, belong to the widely used prior art,
Specific structure those skilled in the art of control module machine can test to obtain required technology and open by limited times according to actual needs
Show, circuit connecting mode those skilled in the art can obtain Technical Reference by consulting the relevant technologies handbook, herein not in detail
The component of explanation is the prior art.
Although above-mentioned be explained in detail specific embodiment of the utility model, the utility model is not limited to
Embodiment is stated, within the knowledge of a person skilled in the art, the utility model aims can also not departed from
Under the premise of make a variety of changes, without have the modification of creative work or deformation still the protection scope of the utility model with
It is interior.
Claims (3)
1. one kind has heat sinking function plant protection drone, including drone body (1), lithium battery (4), winged control module (5), power
Module (6), internal drone body (1) is hollow structure, and lithium battery (4), winged control module (5), power plant module (6) are located at nobody
Machine ontology (1) is internal, lithium battery (4) with fly control module (5), power plant module (6) is connect, which is characterized in that further include it is annular every
Plate (2), cooling tube (3), radiator (7), wherein the annular partition (2) is located at drone body (1) inside, the cooling
Pipe (3) is located at drone body (1) inner wall and annular partition (2) is intermediate, and the radiator (7) is located at drone body (1)
Interior rear portion.
2. according to claim 1 a kind of with heat sinking function plant protection drone, it is characterised in that: the radiator
(7) include outlet tube (701), inlet tube (702), baffle (703), hygrosensor (704), pump (705), check valve (706),
Cooling piece (707), pipeline (708), wherein radiator (7) is divide into upper part and lower part by the baffle (703), the cooling piece
(707) it is located at baffle (703) upper surface, the hygrosensor (704) is located at radiator (7) internal upper part left side wall, described
Pipeline (708) is connected to radiator (7) two parts up and down, installs check valve (706) on the pipeline (708), the outlet tube
(701) it is located at radiator (7) upper half rear wall, the inlet tube (702) is located at radiator (7) lower half rear wall, described
Cooling tube (3) upper port is connect with outlet tube (701), and cooling tube (3) lower port is connect with inlet tube (702), the pump
(705) it is connect with inlet tube (702), the pump (705), cooling piece (707) are connect with control module (5) is flown, the temperature sensing
Device (704) is connect with control module (5) is flown.
3. according to claim 1 a kind of with heat sinking function plant protection drone, it is characterised in that: the cooling tube (3)
For helical form, material is conduction copper.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201920128850.8U CN209581865U (en) | 2019-01-29 | 2019-01-29 | One kind having heat sinking function plant protection drone |
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CN201920128850.8U CN209581865U (en) | 2019-01-29 | 2019-01-29 | One kind having heat sinking function plant protection drone |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2021217545A1 (en) * | 2020-04-30 | 2021-11-04 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
CN115191198A (en) * | 2022-07-28 | 2022-10-18 | 西安宇翼星智能科技有限公司 | Multifunctional automatic material mixing and fertilizing bin device for agricultural unmanned aerial vehicle |
-
2019
- 2019-01-29 CN CN201920128850.8U patent/CN209581865U/en active Active
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2021217545A1 (en) * | 2020-04-30 | 2021-11-04 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
CN115191198A (en) * | 2022-07-28 | 2022-10-18 | 西安宇翼星智能科技有限公司 | Multifunctional automatic material mixing and fertilizing bin device for agricultural unmanned aerial vehicle |
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