CN205418117U - Letter way plant protection unmanned aerial vehicle with from inhaling medicine system of spouting - Google Patents
Letter way plant protection unmanned aerial vehicle with from inhaling medicine system of spouting Download PDFInfo
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- CN205418117U CN205418117U CN201620206914.8U CN201620206914U CN205418117U CN 205418117 U CN205418117 U CN 205418117U CN 201620206914 U CN201620206914 U CN 201620206914U CN 205418117 U CN205418117 U CN 205418117U
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Abstract
The utility model relates to a plant protection unmanned aerial vehicle specifically is a letter way plant protection unmanned aerial vehicle with from inhaling medicine system of spouting. The utility model provides a problem that current plant protection unmanned aerial vehicle energy consumption is high, the operating efficiency is low. Letter way plant protection unmanned aerial vehicle with from inhaling medicine system of spouting, including rack section, fuselage part, certainly inhale spout the medicine part, the machine carries equipment part, the rack section includes skid, stand, crossbeam, upper platform, middle level platform, lower floor's platform, the fuselage part is including cross horn, the hyperbola letter way body, motor, screw, spout the medicine part including medical kit, vertical loading pipe, the horizontal loading pipe of cross, liquid drug spraying nozzle, electronic speed regulating valve from inhaling, the machine carries equipment part and includes power battery, electronic equipment storehouse. The utility model is suitable for a plant protection field.
Description
Technical field
This utility model relates to plant protection unmanned plane, a kind of exhausting plant protection unmanned plane with self-priming pesticide spraying system.
Background technology
Plant protection unmanned plane is widely used in plant protection field.Under prior art conditions, plant protection unmanned plane generally has for medicine sprinkling system.But practice have shown that, owing to being limited for the structure of medicine sprinkling system by it, generally there is the problem that energy consumption is high, working performance is low in existing plant protection unmanned plane.Specifically, the medicine sprinkling system that supplies of existing plant protection unmanned plane all uses electric booster pump to realize conveying and the sprinkling of medicinal liquid, in order to ensure that electric booster pump normally works, need on plant protection unmanned plane to be equipped with and storage battery dedicated power for electric booster pump, thus bring following problem: one, add the energy consumption of plant protection unmanned plane.Its two, owing to storage battery dedicated weight is the biggest so that the load of plant protection unmanned plane is very big, thus cause that its hang time is short, landing often, thus causes its working performance low.Based on this, it is necessary to invent a kind of brand-new plant protection unmanned plane, to solve the problems referred to above that existing plant protection unmanned plane exists.
Summary of the invention
This utility model is in order to solve the problem that existing plant protection unmanned plane energy consumption is high, working performance is low, it is provided that a kind of exhausting plant protection unmanned plane with self-priming pesticide spraying system.
This utility model adopts the following technical scheme that realization:
There is the exhausting plant protection unmanned plane of self-priming pesticide spraying system, including rack section, fuselage sections, self-priming spray medicine part, airborne equipment part；
Described rack section includes skid, column, crossbeam, upper platform, middle level platform, lower floor's platform；The number of skid is two；Two skids are in the most arranged in parallel；The number of column is four；Four root posts are parallel to each other, and the rectangular arrangement of four root posts；The lower end of four root posts is respectively perpendicular left part and the right part being fixed on two skids；The number of crossbeam is two；Two crossbeams are that left and right is arranged in parallel；The front-end and back-end of two crossbeams are respectively perpendicular the upper end being fixed on four root posts；Upper platform, middle level platform, lower floor's platform are the most arranged in parallel；The lower surface left part of upper platform and lower surface right part are individually fixed in the middle part of two crossbeams；Four corners of middle level platform are individually fixed in the middle part of four root posts；Four corners of lower floor's platform are individually fixed in the bottom of four root posts；
Described fuselage sections includes cross horn, hyperbola exhausting body, motor, propeller；The lower surface of upper platform is fixed in the central authorities of cross horn；The number of hyperbola exhausting body is four；Four limits of cross horn extend through the side being fixed on four hyperbola exhausting bodies, and four ends of cross horn lay respectively at the inner chamber central authorities of four hyperbola exhausting bodies；The number of motor is four；Four motors are respectively arranged in four ends of cross horn；The number of propeller is four；The oar axle of four propellers output shaft with four motors respectively is connected；
Described self-priming spray medicine part includes medicine-chest, vertical grug transportation tube, the horizontal grug transportation tube of cross, liquid nozzle, electronic speed regulation valve；Medicine-chest is installed on the upper surface of lower floor's platform；The lower end of vertical grug transportation tube and the inner space of medicine-chest；The central authorities of the horizontal grug transportation tube of cross connect with the upper end of vertical grug transportation tube；Four limits of the horizontal grug transportation tube of cross extend through the waist side being fixed on four hyperbola exhausting bodies, and the horizontal grug transportation tube of cross is positioned at the underface of cross horn；The number of liquid nozzle is four；Four liquid nozzles are respectively arranged in four ends of the horizontal grug transportation tube of cross；Electronic speed regulation valve is installed on vertical grug transportation tube；
Described airborne equipment part includes electrokinetic cell, electronic equipment storehouse；Electrokinetic cell is installed on the upper surface of upper platform；The outfan energization input respectively with four motors of powering of electrokinetic cell is connected；Electronic equipment storehouse is installed on the lower surface of upper platform.
During work, in medicine-chest, store medicinal liquid.The inner chamber in electronic equipment storehouse is provided with flight control system.The control output end of flight control system is connected with control input, the control input of electronic speed regulation valve of four motors respectively.Ground staff sends remote signal to flight control system, and flight control system controls four motors respectively according to the remote signal received and rotates, and controls electronic speed regulation valve and carry out action.Specific works process is as follows: four motors drive four propellers to rotate respectively, and makes to there is speed discrepancy between four propellers, and on the one hand four propellers thus provide horizontal propulsive force, on the other hand provide vertical lift.Change by controlling the speed discrepancy between four propellers, i.e. controllable levels propulsive force and the size of vertical lift.Under the common effect of vertical lift and horizontal propulsive force, plant protection unmanned plane can realize various flare maneuver (such as advance, retreat, left and right turn, pivot stud etc.).When plant protection unmanned plane during flying to dispenser place, electronic speed regulation valve is opened.Now, the high velocity air (high velocity air is rotated by four propellers and produces, and fastest when flowing through the waist of hyperbola exhausting body) in four hyperbola exhausting bodies flows separately through at four liquid nozzles, and forms negative pressure respectively at four liquid nozzles.Under the self-priming effect of negative pressure, medicinal liquid in medicine-chest passes sequentially through vertical grug transportation tube, the horizontal grug transportation tube of cross is delivered to four liquid nozzles respectively, and spray through four liquid nozzles respectively, it is sprayed onto plant surface then as the high velocity air in four hyperbola exhausting bodies, is achieved in dispenser operation.
Based on said process, compared with existing plant protection unmanned plane, the exhausting plant protection unmanned plane with self-priming pesticide spraying system described in the utility model is without using electric booster pump (i.e. without be equipped with storage battery dedicated power for electric booster pump), and the self-priming effect of negative pressure only need to be utilized can to realize conveying and the sprinkling of medicinal liquid, thus it has possessed following advantage: one, due to storage battery dedicated without being equipped with, this utility model significantly reduces self energy consumption.Its two, due to storage battery dedicated without being equipped with, this utility model greatly reduces self load, the most significantly extends the hang time, landing number of times is greatly reduced, thus working performance is greatly improved.
This utility model is rational in infrastructure, it is ingenious to design, and efficiently solves the problem that existing plant protection unmanned plane energy consumption is high, working performance is low, it is adaptable to plant protection field.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
Fig. 2 is the top view of Fig. 1.
In figure: 10-skid, 11-column, 12-crossbeam, 13-upper platform, 14-middle level platform, 15-lower floor platform, 20-cross horn, 21-hyperbola exhausting body, 22-motor, 23-propeller, 30-medicine-chest, the vertical grug transportation tube of 31-, the horizontal grug transportation tube of 32-cross, 33-liquid nozzle, 34-electronic speed regulation valve, 40-electrokinetic cell, 41-electronic equipment storehouse.
Detailed description of the invention
There is the exhausting plant protection unmanned plane of self-priming pesticide spraying system, including rack section, fuselage sections, self-priming spray medicine part, airborne equipment part；
Described rack section includes skid 10, column 11, crossbeam 12, upper platform 13, middle level platform 14, lower floor's platform 15；The number of skid 10 is two；Two skids 10 are in the most arranged in parallel；The number of column 11 is four；Four root posts 11 are parallel to each other, and the four rectangular arrangements of root post 11；The lower end of four root posts 11 is respectively perpendicular left part and the right part being fixed on two skids 10；The number of crossbeam 12 is two；Two crossbeams 12 are arranged in parallel in left and right；The front-end and back-end of two crossbeams 12 are respectively perpendicular the upper end being fixed on four root posts 11；Upper platform 13, middle level platform 14, lower floor's platform 15 are the most arranged in parallel；The lower surface left part of upper platform 13 and lower surface right part are individually fixed in the middle part of two crossbeams 12；Four corners of middle level platform 14 are individually fixed in the middle part of four root posts 11；Four corners of lower floor's platform 15 are individually fixed in the bottom of four root posts 11；
Described fuselage sections includes cross horn 20, hyperbola exhausting body 21, motor 22, propeller 23；The lower surface of upper platform 13 is fixed in the central authorities of cross horn 20；The number of hyperbola exhausting body 21 is four；Four limits of cross horn 20 extend through the side being fixed on four hyperbola exhausting bodies 21, and four ends of cross horn 20 lay respectively at the inner chamber central authorities of four hyperbola exhausting bodies 21；The number of motor 22 is four；Four motors 22 are respectively arranged in four ends of cross horn 20；The number of propeller 23 is four；The oar axle of four propellers 23 output shaft with four motors 22 respectively is connected；
Described self-priming spray medicine part includes medicine-chest 30, vertical grug transportation tube 31, the horizontal grug transportation tube of cross 32, liquid nozzle 33, electronic speed regulation valve 34；Medicine-chest 30 is installed on the upper surface of lower floor's platform 15；The lower end of vertical grug transportation tube 31 and the inner space of medicine-chest 30；The central authorities of the horizontal grug transportation tube of cross 32 connect with the upper end of vertical grug transportation tube 31；Four limits of the horizontal grug transportation tube of cross 32 extend through the waist side being fixed on four hyperbola exhausting bodies 21, and the horizontal grug transportation tube of cross 32 is positioned at the underface of cross horn 20；The number of liquid nozzle 33 is four；Four liquid nozzles 33 are respectively arranged in four ends of the horizontal grug transportation tube of cross 32；Electronic speed regulation valve 34 is installed on vertical grug transportation tube 31；
Described airborne equipment part includes electrokinetic cell 40, electronic equipment storehouse 41；Electrokinetic cell 40 is installed on the upper surface of upper platform 13；The outfan energization input respectively with four motors 22 of powering of electrokinetic cell 40 is connected；Electronic equipment storehouse 41 is installed on the lower surface of upper platform 13.
When being embodied as, the power of four motors 22 is identical.The consistent size of four propellers 23.
Claims (1)
1. an exhausting plant protection unmanned plane with self-priming pesticide spraying system, it is characterised in that: include that rack section, fuselage sections, self-priming spray medicine part, airborne equipment part；
Described rack section includes skid (10), column (11), crossbeam (12), upper platform (13), middle level platform (14), lower floor's platform (15)；The number of skid (10) is two；Two skids (10) are in the most arranged in parallel；The number of column (11) is four；Four root posts (11) are parallel to each other, and four root posts (11) rectangular arrangement；The lower end of four root posts (11) is respectively perpendicular left part and the right part being fixed on two skids (10)；The number of crossbeam (12) is two；Two crossbeams (12) are arranged in parallel in left and right；The front-end and back-end of two crossbeams (12) are respectively perpendicular the upper end being fixed on four root posts (11)；Upper platform (13), middle level platform (14), lower floor's platform (15) are the most arranged in parallel；The lower surface left part of upper platform (13) and lower surface right part are individually fixed in the middle part of two crossbeams (12)；Four corners of middle level platform (14) are individually fixed in the middle part of four root posts (11)；Four corners of lower floor's platform (15) are individually fixed in the bottom of four root posts (11)；
Described fuselage sections includes cross horn (20), hyperbola exhausting body (21), motor (22), propeller (23)；The lower surface of upper platform (13) is fixed in the central authorities of cross horn (20)；The number of hyperbola exhausting body (21) is four；Four limits of cross horn (20) extend through the side being fixed on four hyperbolies exhausting body (21), and four ends of cross horn (20) lay respectively at the inner chamber central authorities of four hyperbolies exhausting body (21)；The number of motor (22) is four；Four motors (22) are respectively arranged in four ends of cross horn (20)；The number of propeller (23) is four；The oar axle of four propellers (23) output shaft with four motors (22) respectively is connected；
Described self-priming spray medicine part includes medicine-chest (30), vertical grug transportation tube (31), the horizontal grug transportation tube of cross (32), liquid nozzle (33), electronic speed regulation valve (34)；Medicine-chest (30) is installed on the upper surface of lower floor's platform (15)；The lower end of vertical grug transportation tube (31) and the inner space of medicine-chest (30)；The central authorities of the horizontal grug transportation tube of cross (32) connect with the upper end of vertical grug transportation tube (31)；Four limits of the horizontal grug transportation tube of cross (32) extend through the waist side being fixed on four hyperbolies exhausting body (21), and the horizontal grug transportation tube of cross (32) is positioned at the underface of cross horn (20)；The number of liquid nozzle (33) is four；Four liquid nozzles (33) are respectively arranged in four ends of the horizontal grug transportation tube of cross (32)；Electronic speed regulation valve (34) is installed on vertical grug transportation tube (31)；
Described airborne equipment part includes electrokinetic cell (40), electronic equipment storehouse (41)；Electrokinetic cell (40) is installed on the upper surface of upper platform (13)；The power supply outfan of electrokinetic cell (40) energization input with four motors (22) respectively is connected；Electronic equipment storehouse (41) is installed on the lower surface of upper platform (13).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620206914.8U CN205418117U (en) | 2016-03-17 | 2016-03-17 | Letter way plant protection unmanned aerial vehicle with from inhaling medicine system of spouting |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620206914.8U CN205418117U (en) | 2016-03-17 | 2016-03-17 | Letter way plant protection unmanned aerial vehicle with from inhaling medicine system of spouting |
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| CN205418117U true CN205418117U (en) | 2016-08-03 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620206914.8U Expired - Fee Related CN205418117U (en) | 2016-03-17 | 2016-03-17 | Letter way plant protection unmanned aerial vehicle with from inhaling medicine system of spouting |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108849806A (en) * | 2018-04-12 | 2018-11-23 | 河南大诚通用航空科技有限公司 | A kind of plant protection drone spray tank with liquid isolation capsule |
-
2016
- 2016-03-17 CN CN201620206914.8U patent/CN205418117U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108849806A (en) * | 2018-04-12 | 2018-11-23 | 河南大诚通用航空科技有限公司 | A kind of plant protection drone spray tank with liquid isolation capsule |
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| Date | Code | Title | Description |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 030603, Shanxi Jinzhong District, Yuci Yingbin West Street and Tian commercial building 5 Patentee after: Shanxi Shipule General Aviation Technology Co. Ltd. Address before: 030603, Shanxi Jinzhong District, Yuci Yingbin West Street and Tian commercial building 5 Patentee before: SHANXI SHIPULE AVIATION PLANT PROTECTION TECHNOLOGY CO., LTD. |
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160803 Termination date: 20170317 |
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| CF01 | Termination of patent right due to non-payment of annual fee |