CN203612209U - Agricultural aircraft - Google Patents
Agricultural aircraft Download PDFInfo
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- CN203612209U CN203612209U CN201320753949.XU CN201320753949U CN203612209U CN 203612209 U CN203612209 U CN 203612209U CN 201320753949 U CN201320753949 U CN 201320753949U CN 203612209 U CN203612209 U CN 203612209U
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- pipe
- subpanel
- agricultural aircraft
- agricultural
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Abstract
The utility model provides an agricultural aircraft which is compact in structure, reasonable in design, and high in efficiency, realizes uniform spraying, and can conveniently carry a pesticide. The agricultural aircraft comprises a mounting plate, eight connecting rods, eight propellers, a mounting frame and an infusion pump, wherein a control device mounting part is arranged in the center of the mounting plate; one end of each of the connecting rods is mounted on the outer periphery of the mounting plate, and the other end of the connecting rod is connected with a motor through a motor base; the eight propellers are connected with the motors; the mounting frame is arranged below the mounting plate, and a storage battery and a pesticide box are mounted on the mounting frame; the infusion pump is arranged in the pesticide box; the output end of the infusion pump is connected with one end of an infusion pipe, and the other end of the infusion pipe is connected with a sprayer.
Description
Technical field
The utility model relates to equipment for plant protection technical field, is specifically related to a kind of agricultural aircraft.
Background technology
The many rotor unmanned aircrafts of current eight axle, because flight stability, lightweight, landing are not subject to the features such as place restriction, are widely current, for spraying insecticide on market.
Ubiquity motor pulling force is little, structure is little, load-bearing is generally less than 15 kilograms and the shortcoming such as production time is short.
Utility model content
The utility model object is to provide that a kind of structure is closely gathered, reasonable in design, efficiency is high, sprinkling is even, carry agricultural chemicals agricultural aircraft easily.
To achieve these goals, the utility model adopts technical scheme as follows:
A kind of agricultural aircraft, comprising:
One subpanel, center is control setup installation portion;
Eight pipe links, each pipe link one end is arranged on subpanel outside, and the other end is provided with motor by motor cabinet;
Eight screw propellers, are connected with motor;
Erecting frame, is arranged on subpanel below, and storage battery and medicine-chest is installed; With
Infusion pump, is arranged in medicine-chest, and transfusion delivery side of pump connects the defeated one end of hydraulic pipe, and the hydraulic pipe other end is connected with shower nozzle.
Above-mentioned agricultural aircraft, screw propeller forms downward-sloping state along direction and the horizontal surface of propeller blade, and angle of inclination is at 3-5 °.
Above-mentioned agricultural aircraft, is provided with flight controller, GPS navigation instrument, GPS module, signal projector and data-interface in control setup installation portion; Wherein GPS module, signal projector 33 and data-interface are all connected with flight controller, and GPS module is connected with GPS navigation instrument; Flight controller is connected with motor by pressure regulator; Agricultural also comprises with aircraft the control cabin that is provided with computing machine, and computing machine is connected with signal receiving processor.
Above-mentioned agricultural aircraft, control setup installation portion is also provided with camera, and camera is connected with flight controller.
Above-mentioned agricultural aircraft, erecting frame comprises the bend pipe of falling U of two parallel interval settings, for connecting the connection pipe of the bend pipe of falling U end and the reinforced pipe between two bend pipes of falling U, on two bend pipe of falling U tops, underframe attaching parts is installed, on underframe attaching parts, be integrated through pipe link serial connection, pipe link is fixed on subpanel bottom surface through clamping hoop type attaching parts.
Above-mentioned agricultural aircraft, subpanel is circular ring structure, along the uniform multiple through holes of annular radii direction, described through hole is inserted in one end that pipe link is connected with subpanel, and with through hole be interference fit.
Above-mentioned agricultural aircraft, subpanel and motor cabinet are aviation aluminium.
Above-mentioned agricultural aircraft, pipe link, erecting frame and screw propeller material are carbon fiber.
The beneficial effects of the utility model:
Structure is closely gathered, reasonable in design, efficiency is high, sprinkling is even, cost is low; Medicine-chest and erecting frame are integrated, can be more stable carry agricultural chemicals, the accident that while having stopped navigation, medicine-chest comes off occurs, and has also reduced due to harmful effect unstable and that fuselage is produced.
Accompanying drawing explanation
Fig. 1 is the schematic perspective view of the selected embodiment of the utility model.
Fig. 2 is that the master of the selected embodiment of the utility model looks schematic diagram.
Fig. 3 is the control setup schematic diagram of the selected embodiment of the utility model.
Fig. 4 is the erecting frame structural representation of the selected embodiment of the utility model.
In figure 1, subpanel, 2, attaching parts, 3, underframe attaching parts, 4, pipe link, 5, erecting frame, 6, water tank, 7, pipe link, 8, motor cabinet, 9, motor, 10, screw propeller, 11, infusion pump, 12, shower nozzle, 13, control setup installation portion, 14, GPS navigation instrument, 15, camera, 16, storage battery, 17, pressure regulator, 18, flight controller, 19, GPS module, 20, signal projector, 21, data-interface, 22, control cabin, 23, computing machine, 24, signal receiving processor.
The specific embodiment
Better understand the utility model for the ease of those skilled in the art, below in conjunction with the drawings and specific embodiments, the utility model is described in further details, following is only the exemplary protection domain of the present utility model that do not limit.
With reference to accompanying drawing 1, a kind of agricultural aircraft, comprises subpanel 11, eight pipe links 7, eight screw propellers 10, eight motors 9, erecting frame 5, storage battery 16 and medicine-chests 6; Subpanel 1 center is control setup installation portion 13; Each pipe link 7 one end are arranged on subpanel 1 outside, and the other end is provided with motor 9 by motor cabinet 8; Screw propeller 10 is connected with motor 9; Erecting frame 5 is arranged on subpanel 1 below, and is connected with pipe link 7, and storage battery 16 and medicine-chest 6 are installed; In medicine-chest 6, be provided with infusion pump 11, the mouth of infusion pump 11 connects the defeated one end of hydraulic pipe, and the hydraulic pipe other end is connected with shower nozzle 12.
With reference to accompanying drawing 2, screw propeller 10 forms downward-sloping state along direction and the horizontal surface of screw propeller 10 blades, and angle of inclination a, at 3-5 °, can increase the stability of aircraft.
With reference to accompanying drawing 3, in control setup installation portion, be provided with flight controller 18, GPS navigation instrument 14, GPS module 19, signal projector 20 and data-interface 21; Wherein GPS module 19, signal projector 20 and data-interface 21 are all connected with flight controller 18, and GPS module 19 is connected with GPS navigation instrument 14; Flight controller logical 18 is crossed pressure regulator 17 and is connected with motor 9; Agricultural also comprises with aircraft the control cabin 22 that is provided with computing machine 23, and computing machine 23 is connected with signal receiving processor 24.
With reference to accompanying drawing 1,3, control setup installation portion 13 is also provided with camera 15, and camera 15 is connected with flight controller 18.
With reference to accompanying drawing 4, erecting frame 5 comprises the bend pipe of falling U 501 of two parallel interval settings, for connecting the connection pipe 503 of the bend pipe of falling U 501 ends and the reinforced pipe 502 between two bend pipes of falling U 501.On two bend pipe of falling U 501 tops, underframe attaching parts 3 is installed, on underframe attaching parts 3, is integrated through pipe link 4 serial connections, pipe link 4 is fixed on subpanel 11 bottom surfaces through clamping hoop type attaching parts 2.
In the present embodiment, subpanel 1 is circular ring structure, and along the uniform multiple through holes of annular radii direction, described through hole is inserted in one end that pipe link 7 is connected with subpanel 1.
In the present embodiment, subpanel 1 and motor cabinet 8 is aviation aluminium, and intensity is high, lightweight, effectively alleviated aircraft own wt, and its load-carrying capacity is strengthened; Pipe link 7, erecting frame 5 and screw propeller 10 materials are carbon fiber, and intensity is high, lightweight, extended service life.
Below only described groundwork of the present utility model and preferred implementation, those skilled in the art can make many changes and improvements according to foregoing description, and these changes and improvements should belong to protection domain of the present utility model.
Claims (8)
1. an agricultural aircraft, is characterized in that comprising:
One subpanel, center is control setup installation portion;
Eight pipe links, each pipe link one end is arranged on subpanel outside, and the other end is provided with motor by motor cabinet;
Eight screw propellers, are connected with motor;
Erecting frame, is arranged on subpanel below, and storage battery and medicine-chest is installed; With
Infusion pump, is arranged in medicine-chest, and transfusion delivery side of pump connects hydraulic pipe one end, and the hydraulic pipe other end is connected with shower nozzle.
2. agricultural aircraft according to claim 1, is characterized in that: screw propeller forms downward-sloping state along direction and the horizontal surface of propeller blade, and angle of inclination is at 3-5 °.
3. agricultural aircraft according to claim 1, is characterized in that: in control setup installation portion, be provided with flight controller, GPS navigation instrument, GPS module, signal projector and data-interface; Wherein GPS module, signal projector and data-interface are all connected with flight controller, and GPS module is connected with GPS navigation instrument; Flight controller is connected with motor by pressure regulator; Agricultural also comprises with aircraft the control cabin that is provided with computing machine, and computing machine is connected with signal receiving processor.
4. agricultural aircraft according to claim 3, is characterized in that: control setup installation portion is also provided with camera, camera is connected with flight controller.
5. agricultural aircraft according to claim 1, it is characterized in that: erecting frame comprises the bend pipe of falling U of two parallel interval settings, for connecting the connection pipe of the bend pipe of falling U end and the reinforced pipe between two bend pipes of falling U, on two bend pipe of falling U tops, underframe attaching parts is installed, on underframe attaching parts, be integrated through pipe link serial connection, pipe link is fixed on subpanel bottom surface through clamping hoop type attaching parts.
6. according to agricultural aircraft described in claim 1 to 5 any one, it is characterized in that: subpanel is circular ring structure, along the uniform multiple through holes of annular radii direction, described through hole is inserted in one end that pipe link is connected with subpanel, and with through hole be interference fit.
7. according to agricultural aircraft described in claim 1 to 5 any one, it is characterized in that: subpanel and motor cabinet are aviation aluminium.
8. according to agricultural aircraft described in claim 1 to 5 any one, it is characterized in that: pipe link, erecting frame and screw propeller material are carbon fiber.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320753949.XU CN203612209U (en) | 2013-11-26 | 2013-11-26 | Agricultural aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320753949.XU CN203612209U (en) | 2013-11-26 | 2013-11-26 | Agricultural aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203612209U true CN203612209U (en) | 2014-05-28 |
Family
ID=50764869
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320753949.XU Expired - Fee Related CN203612209U (en) | 2013-11-26 | 2013-11-26 | Agricultural aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203612209U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104494816A (en) * | 2014-12-05 | 2015-04-08 | 成都盛世普益科技有限公司 | Unmanned aerial vehicle specially used for spraying field ridge herbicide |
| CN104782603A (en) * | 2015-04-10 | 2015-07-22 | 尖蜂航空科技有限公司 | Foldable multi-rotor-wing plant protection plane |
| CN105253303A (en) * | 2015-10-23 | 2016-01-20 | 杨珊珊 | Device and method for regulating unmanned aerial vehicle spray range |
| CN105752340A (en) * | 2016-04-07 | 2016-07-13 | 广州极飞电子科技有限公司 | Unmanned aerial vehicle |
| CN106614481A (en) * | 2017-01-04 | 2017-05-10 | 四川克瑞斯航空科技有限公司 | Drone-based controllable pesticide spraying system |
| CN108033017A (en) * | 2017-12-26 | 2018-05-15 | 山东绿风农业集团有限公司 | A kind of agricultural aircraft |
-
2013
- 2013-11-26 CN CN201320753949.XU patent/CN203612209U/en not_active Expired - Fee Related
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104494816A (en) * | 2014-12-05 | 2015-04-08 | 成都盛世普益科技有限公司 | Unmanned aerial vehicle specially used for spraying field ridge herbicide |
| CN104494816B (en) * | 2014-12-05 | 2016-04-13 | 宁波达鹏无人机科技有限公司 | Be exclusively used in the unmanned plane spraying field stalk herbicide |
| CN104782603A (en) * | 2015-04-10 | 2015-07-22 | 尖蜂航空科技有限公司 | Foldable multi-rotor-wing plant protection plane |
| CN104782603B (en) * | 2015-04-10 | 2017-07-11 | 东营黄蓝知识产权运营管理有限公司 | Foldable many rotor fog machines |
| CN105253303A (en) * | 2015-10-23 | 2016-01-20 | 杨珊珊 | Device and method for regulating unmanned aerial vehicle spray range |
| CN105752340A (en) * | 2016-04-07 | 2016-07-13 | 广州极飞电子科技有限公司 | Unmanned aerial vehicle |
| CN105752340B (en) * | 2016-04-07 | 2017-09-01 | 广州极飞科技有限公司 | Unmanned vehicle |
| CN106614481A (en) * | 2017-01-04 | 2017-05-10 | 四川克瑞斯航空科技有限公司 | Drone-based controllable pesticide spraying system |
| CN108033017A (en) * | 2017-12-26 | 2018-05-15 | 山东绿风农业集团有限公司 | A kind of agricultural aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| ASS | Succession or assignment of patent right |
Owner name: SHANDONG TIANXI AVIATION TECHNOLOGY CO., LTD. Free format text: FORMER OWNER: SHANDONG NEW MORNING TECHNOLOGY CO., LTD. Effective date: 20150424 |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20150424 Address after: 253000, No. 5-7, A District, Dong Zi Culture Street, 1118 Dongfanghong Road, Dezhou Economic Development Zone, Shandong, China Patentee after: Shandong Tianxi Aviation Technology Co. Ltd. Address before: 253000, No. 301, building 2, building 13, Fifth Ring Road, Youth League Road, Decheng District, Dezhou City, Shandong Province, China, No. 3 Patentee before: SHANDONG XINCHEN TECHNOLOGY CO., LTD. |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20190826 Address after: 253000 Shandong Dezhou Economic and Technological Development Zone Changhe Street Office, No. 10th Floor 1009, Donghui Building, Business Center, North of March 8th East Road Patentee after: Dezhou Hongbo Network Technology Co., Ltd. Address before: 253000, No. 5-7, A District, Dong Zi Culture Street, 1118 Dongfanghong Road, Dezhou Economic Development Zone, Shandong, China Patentee before: Shandong Tianxi Aviation Technology Co. Ltd. |
|
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20140528 Termination date: 20191126 |