CN205293080U - Four electronic rotors agricultural plant protection unmanned aerial vehicle - Google Patents
Four electronic rotors agricultural plant protection unmanned aerial vehicle Download PDFInfo
- Publication number
- CN205293080U CN205293080U CN201620022229.XU CN201620022229U CN205293080U CN 205293080 U CN205293080 U CN 205293080U CN 201620022229 U CN201620022229 U CN 201620022229U CN 205293080 U CN205293080 U CN 205293080U
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- pump chamber
- control room
- unmanned plane
- electromechanical control
- motor
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Abstract
The utility model belongs to the technical field of the agricultural aviation plant protection, especially, relate to a four electronic rotors agricultural plant protection unmanned aerial vehicle, electromechanical control room (1) links to each other with four motor cabin (10) through four wing (2) that each other become 90 degrees, and paddle (3) link to each other with the motor of installing in motor cabin (10) lining, pump chamber (4) is connected to electromechanical control room (1) bottom, and pump chamber (4) bottom is annular cavity, cup joints the top of medical kit (5), and pump chamber (4) left and right sides is passed through spray lance (6) and is linked to each other with shower nozzle (7), the bottom of pump chamber (4) is installed four and each other is become 90 degrees undercarriage (8), pilot lamp (9) install in electromechanical control room (1) insidely through side aperture printing opacity. The utility model discloses a medical kit and pump chamber suit structure make things convenient for the medical kit to dismantle and wash, have shortened transfer line length, and the outward appearance adopts streamlined design, and night vision fluorescent material is coated to the spray lance, can operation when the low visibility, and the extension activity duration, eighth circumference's optimalarc support is adopted to the undercarriage bottom, guarantees aircraft descend steady unlikely slope and weight reduction.
Description
Technical field
This utility model belongs to agricultural aviation plant protection technology field, particularly relates to a kind of electronic four rotor agricultural plant protection unmanned planes.
Background technology
Agricultural aviation plant protection technology improves Crop in China prevention and control of plant diseases, pest control Mechanization Level as the important component part of modern agriculture and reflection agricultural modernization level a pair of important symbol, carry out the proficient service of Unifying control, improve the utilization rate of agricultural resource, strengthen sudden large area pest and disease damage prevention and control ability, alleviate rural laborer's shortage, strengthen the agricultural ability to ward off risks, ensure national food security, ecological safety, it is achieved agricultural sustainable development tool is of great significance.
Plant protection unmanned plane mainly has two kinds of types in the market: the dynamic single-blade leaf helicopter of oil and electronic many blades unmanned plane. The multidigit expert of agricultural aviation industrial technology innovation strategic alliances of China has carried out multinomial experiment, and research shows that electronic many blades unmanned plane is more suitable for plant protection operation. Electronic many blades unmanned plane common are four axles, six axles, eight axles. Compared with single shaft single-blade leaf depopulated helicopter, its structure has very big-difference, and multiple blades are generally adopted circular symmetric structure layout, all adopts battery power to drive, and produced air-flow is the coefficient result of multiple blade in-flight. The circular unmanned unmanned plane of multi-shaft, multi-propeller leaf except have operation height low, can VTOL, without special landing airport, the outstanding advantages such as flexible operation is light, environmental suitability is strong except, compared with single shaft single-blade leaf depopulated helicopter, also have that frame for movement is simpler, foldable dismounting, flight more steadily, degree of modularity high.
Domestic existing electronic many blades unmanned plane adopts easy multiaxis carbon fibre supporting structure mostly in order to alleviate deadweight, this simple in construction, from heavy and light, easily install, quick detachable, but as plant protection aircraft, due to the general all poisonous and harmfuls of pesticide, circuit cause the reasons such as corrosion can be substantially reduced the reliability of aircraft.
The aviation plant protection unmanned plane having at present have employed enclosed structure, controls to be individually enclosed in control room and pump chamber with telecommunication circuit and battery, Teat pipette, eliminates the contact of water or pesticide, be effectively improved reliability. But control room and medicine-chest are connected together and can not dismantle, and changing dressings is injected by dosing mouth, and therefore medicine-chest cannot dismantle thorough cleaning, can only rinse from water inlet water filling. Additionally, medicine-chest is in the middle of control room and pump chamber, though medicine-chest detachably also first to dismantle pump chamber could to unload medicine-chest pretty troublesome. Spray boom is longer can reach 1.5��3 meters, and effective spraying swath reaches 3��6 meters, cannot be directly observed spraying range during dark.
Utility model content
In order to overcome the defect of prior art, the utility model proposes a kind of electronic four rotor agricultural plant protection unmanned planes, including: Electromechanical Control room 1, wing 2, blade 3, pump chamber 4, medicine-chest 5, spray boom 6, shower nozzle 7, undercarriage 8, display lamp 9, motor room 10;
Wherein, Electromechanical Control room 1 is connected with four motor rooms 10 by four wings 2 being mutually 90 degree; Motor room 10 is used to encapsulated motor, and the motor in motor room 10 is connected with blade 3; Connect pump chamber 4 bottom Electromechanical Control room 1, be annular hollow bottom pump chamber 4, the top of socket medicine-chest 5, pump chamber 4 left and right sides is connected with shower nozzle 7 by spray boom 6; The bottom of pump chamber 4 is provided with four undercarriages 8 being mutually 90 degree; Display lamp 9 is installed on inside, Electromechanical Control room 1 and by side aperture.
Spacing distance between the length of described spray boom 6 and the quantity of shower nozzle 7 and multiple shower nozzle 7 is adjusted according to pesticide spraying area.
Described Electromechanical Control room 1 and pump chamber 4 adopt disc-shape airflow design.
Described spray boom 6 scribbles the fluorescent material of night vision function, effectively extends and spray the activity duration, also be adapted for the operation when greasy weather low visibility.
Adopting the arc line shaped support of 1/8th circumferences bottom described undercarriage 8, this design had both ensured that aircraft landing steadily will not tilt, and can make again undercarriage lighter in weight.
Described Electromechanical Control room 1 is by flight control system, electricity tune, receiver, GPS, lithium battery encapsulation together.
Described display lamp is red yellowish green trichromatism LED, is used for showing unmanned plane state: green expression unmanned plane normal condition, and yellow quick flashing represents that electric quantity of lithium battery is not enough, and red expression electricity wretched insufficiency, by air crash.
The beneficial effects of the utility model are in that:
(1) change control room, medicine-chest, pump chamber cascaded structure into medicine-chest and pump chamber sleeve structure, and medicine-chest is detachable, convenient cleaning.
(2), owing to medicine-chest and pump chamber connect together, substantially reduce pesticide box to the transfer line length between pump, be all effective for saving power, reducing deadweight.
(3) circuit control room, pump chamber outward appearance adopt airflow design, have modern sense.
(4) spray boom coats the fluorescent material of night vision function, it is possible in the morning, at dusk operation, effectively extends and sprays the activity duration, also is adapted for the operation when greasy weather low visibility.
(5) adopting the arc line shaped support of 1/8th circumferences bottom undercarriage, this design had both ensured that aircraft landing steadily will not tilt, and can make again undercarriage lighter in weight.
Accompanying drawing explanation
Fig. 1 is the electronic four rotor agricultural plant protection unmanned plane structural representations that the utility model proposes.
Fig. 2 is the top view of Electromechanical Control room.
Fig. 3 is the front view of Electromechanical Control room.
Fig. 4 is the top view of medicine-chest.
Fig. 5 is the front view of medicine-chest.
Fig. 6 is the top view of undercarriage.
Fig. 7 is the front view of undercarriage.
In figure: 1-Electromechanical Control room, 2-wing, 3-blade, 4-pump chamber, 5-medicine-chest, 6-spray boom, 7-shower nozzle, 8-undercarriage, 9-display lamp, 10-motor room.
Detailed description of the invention
Below in conjunction with accompanying drawing, embodiment is elaborated.
As it is shown in figure 1, the utility model proposes a kind of electronic four rotor agricultural plant protection unmanned planes, including: Electromechanical Control room 1, wing 2, blade 3, pump chamber 4, medicine-chest 5, spray boom 6, shower nozzle 7, undercarriage 8, display lamp 9, motor room 10;
Wherein, Electromechanical Control room 1 is connected with four motor rooms 10 by four wings 2 being mutually 90 degree; Motor room 10 is used to encapsulated motor, and the motor in motor room 10 is connected with blade 3; Connect pump chamber 4 bottom Electromechanical Control room 1, be annular hollow bottom pump chamber 4, the top of socket medicine-chest 5, pump chamber 4 left and right sides is connected with shower nozzle 7 by spray boom 6; The bottom of pump chamber 4 is provided with four undercarriages 8 being mutually 90 degree; Display lamp 9 is installed on inside, Electromechanical Control room 1 and by side aperture.
As shown in Figure 2 to 7, wherein, the height of Electromechanical Control room: 124mm, radius: 220mm;
The height of pump chamber: 80mm, outer radii: 270mm, inner radii: 164mm;
For being socketed the thickness of the load support circle of medicine-chest bottom pump chamber: 16mm, outer radii 190mm, inner radii: 164mm;
Medicine-chest: height 146mm; The integral diameter of undercarriage: 694mm, highly: 193mm;
Wing: length 716mm; Driving the motor diameter of blade: 104mm, symmetrical motor shaft is from 1286mm.
The features such as the plant protection unmanned plane that the utility model proposes has working performance height, landing is flexible, easily manipulate, cost is low, every day calculated by 8 hours, it is possible to spray 250��300 mu, and insecticide efficiency is high, the dose of 40% can be reduced compared with artificial dispenser, advantageously reduce pesticide residues.
This embodiment is only this utility model preferably detailed description of the invention; but protection domain of the present utility model is not limited thereto; any those familiar with the art is in the technical scope that this utility model discloses; the change that can readily occur in or replacement, all should be encompassed within protection domain of the present utility model. Therefore, protection domain of the present utility model should be as the criterion with scope of the claims.
Claims (7)
1. electronic four rotor agricultural plant protection unmanned planes, it is characterized in that, including: Electromechanical Control room (1), wing (2), blade (3), pump chamber (4), medicine-chest (5), spray boom (6), shower nozzle (7), undercarriage (8), display lamp (9), motor room (10);
Wherein, Electromechanical Control room (1) is connected with four motor rooms (10) by four wings (2) being mutually 90 degree; Motor room (10) is used to encapsulated motor, and the inner motor of motor room (10) is connected with blade (3); Bottom, Electromechanical Control room (1) connects pump chamber (4), pump chamber (4) bottom is annular hollow, the top of socket medicine-chest (5), pump chamber (4) left and right sides is connected with shower nozzle (7) by spray boom (6); The bottom of pump chamber (4) is provided with four undercarriages (8) being mutually 90 degree; Display lamp (9) is installed on inside, Electromechanical Control room (1) and by side aperture.
2. unmanned plane according to claim 1, it is characterised in that the spacing distance between the length of described spray boom (6) and the quantity of shower nozzle (7) and multiple shower nozzle (7) is adjusted according to pesticide spraying area.
3. unmanned plane according to claim 1, it is characterised in that described Electromechanical Control room (1) and pump chamber (4) adopt disc-shape airflow design.
4. unmanned plane according to claim 1, it is characterised in that scribble the fluorescent material of night vision function on described spray boom (6), effectively extends and sprays the activity duration, also be adapted for the operation when greasy weather low visibility.
5. unmanned plane according to claim 1, it is characterised in that described undercarriage (8) bottom adopts the arc line shaped support of 1/8th circumferences, and this design had both ensured that aircraft landing steadily will not tilt, and can make again undercarriage lighter in weight.
6. unmanned plane according to claim 1, it is characterised in that described Electromechanical Control room (1) is by flight control system, electricity tune, receiver, GPS, lithium battery encapsulation together.
7. unmanned plane according to claim 1, it is characterised in that described display lamp is red yellowish green trichromatism LED, for showing unmanned plane state: green expression unmanned plane normal condition, yellow quick flashing represents that electric quantity of lithium battery is not enough, and red expression electricity wretched insufficiency, by air crash.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620022229.XU CN205293080U (en) | 2016-01-11 | 2016-01-11 | Four electronic rotors agricultural plant protection unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620022229.XU CN205293080U (en) | 2016-01-11 | 2016-01-11 | Four electronic rotors agricultural plant protection unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205293080U true CN205293080U (en) | 2016-06-08 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620022229.XU Expired - Fee Related CN205293080U (en) | 2016-01-11 | 2016-01-11 | Four electronic rotors agricultural plant protection unmanned aerial vehicle |
Country Status (1)
| Country | Link |
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| CN (1) | CN205293080U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106892116A (en) * | 2017-02-27 | 2017-06-27 | 四川雷神空天科技有限公司 | For the flight instruments platform and its system and operational method of plant protection operation |
| CN108739262A (en) * | 2018-06-15 | 2018-11-06 | 胡立波 | A kind of unmanned plane flower-watering device |
| WO2021134964A1 (en) * | 2019-12-31 | 2021-07-08 | 江苏数字鹰科技股份有限公司 | Pesticide spraying device for unmanned aerial vehicle for plant protection |
| CN116921118A (en) * | 2023-09-12 | 2023-10-24 | 山东锐光电子工程科技有限公司 | Intelligent maintenance device and method for power line |
-
2016
- 2016-01-11 CN CN201620022229.XU patent/CN205293080U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106892116A (en) * | 2017-02-27 | 2017-06-27 | 四川雷神空天科技有限公司 | For the flight instruments platform and its system and operational method of plant protection operation |
| CN108739262A (en) * | 2018-06-15 | 2018-11-06 | 胡立波 | A kind of unmanned plane flower-watering device |
| WO2021134964A1 (en) * | 2019-12-31 | 2021-07-08 | 江苏数字鹰科技股份有限公司 | Pesticide spraying device for unmanned aerial vehicle for plant protection |
| CN116921118A (en) * | 2023-09-12 | 2023-10-24 | 山东锐光电子工程科技有限公司 | Intelligent maintenance device and method for power line |
| CN116921118B (en) * | 2023-09-12 | 2023-11-24 | 山东锐光电子工程科技有限公司 | Intelligent maintenance device and method for power line |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160608 Termination date: 20180111 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |