CN103612757B - The solar pilotless plane of rice seedling is shed in a kind of low latitude on rice field - Google Patents
The solar pilotless plane of rice seedling is shed in a kind of low latitude on rice field Download PDFInfo
- Publication number
- CN103612757B CN103612757B CN201310621233.9A CN201310621233A CN103612757B CN 103612757 B CN103612757 B CN 103612757B CN 201310621233 A CN201310621233 A CN 201310621233A CN 103612757 B CN103612757 B CN 103612757B
- Authority
- CN
- China
- Prior art keywords
- rice
- controller
- conductor wire
- solar cell
- solar
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P60/00—Technologies relating to agriculture, livestock or agroalimentary industries
- Y02P60/12—Technologies relating to agriculture, livestock or agroalimentary industries using renewable energies, e.g. solar water pumping
Abstract
The present invention relates to the solar pilotless plane shedding rice seedling in a kind of low latitude on rice field, belong to new forms of energy aeragronomy technical field.Rice seedling throwing has and reduces labor intensity, and saving of labor, province rice seedling bed, economizes kind, water-saving, the advantage increasing production, increase income, has more that speed is fast, the measured feature of matter with unmanned aerial vehicle rice transplanting.Solar light irradiation to be arranged on starboard wing and solar cell generation current on port wing, electric current is by conductor wire, controller input electrical motor, in electrical motor, electric energy converts mechanical energy to, and electrical motor consumes mechanical energy to be ordered about power take-off shaft and two bladed propeller fast rotational, make unmanned aerial vehicle produce flying power.Solar cell generation current on solar light irradiation starboard tailplane and on port tailplane, electric current inputs computer-controlled electrical motor by conductor wire, controller and the autocontrol switch that confluxes, computer-controlled electrical motor is driven according to program and sheds the rotation of rice shoot runner, rice shoot is thrown to the rice field of suitable rice transplanting from shedding rice shoot outlet.
Description
Technical field
The present invention relates to the solar pilotless plane shedding rice seedling in a kind of low latitude on rice field, belong to new forms of energy aeragronomy technical field.
Background technology
The whole world has population over half to take rice as staple food, and China is one of the major country of production and country of consumption of rice in the world.The Monitoring of Paddy Rice Plant Area of China occupies second place of the world, and rice yield occupies first.In recent years, because development of real estate and road construction bring the rice field area in part area to reduce, must improve Rice Cropping technology further increases paddy and always produces, and meets the demand of population growth to rice yield.
Owing to going up year by year by the cost of labour power rice transplanting in rural area, in recent years, there is the planting patterns of rice transplanting in China Partial paddy rice producing region, in the seedling-cultivation plate of seedling factory, first cultivate the rice seedling that root sticks together with little clay, little rice shoot carries out rice transplanting when being in for 2 ~ 4 leaf phase, rice transplanting improves nearly 10 times of work efficiency than rice transplantation by hand, operating efficiency is high, saving of labor, laborsaving, save time, rice transplanting is turned green soon, tillering node is low, many, effective ripe fringe of tillering is many, generally can increase production about 10%, mechanical rice casting is higher than the efficiency of artificial rice transplanting.
In state-owned two ripe up-to-date technologys, a up-to-date technology is solar electrical energy generation, the photoelectric transformation efficiency of crystal silicon solar batteries under solar radiation is close to 20%, among the photoelectric transformation efficiency of part compound solar cell under cloudy low light irradiation is improving constantly, desert solar power station, Coastal beach solar power station, backwoodsman distributed solar energy generating illumination, roof solar distributed photovoltaic power generation solar power apparatus get more and more, in the new forms of energy international fair of Wuxi, spectators have seen the solar power vehicle of exhibition.Another up-to-date technology is unmanned aerial vehicle technology.The navigation of unmanned aerial vehicle, remote sensing, electronic, shooting, Computer Control Technology have greatly improved, and its application has expanded to more and more broader civil area.The body of existing agricultural Medium Plane is large, fuselage heavy, flight turn radius is large, flight cost is high, use engine petrol to provide flying power, discharge a large amount of carbon dioxide, sulphur dioxide and other pernicious gases, deleterious particle thing awing, pollute the air in rural area.
Summary of the invention
The object of the invention is to overcome deficiency of the prior art, the solar pilotless plane shedding rice seedling in a kind of low latitude on rice field is provided.First solar energy generation technology and unmanned aerial vehicle technology are applied in rice transplanting production by the present invention, promote further developing of rice seedling throwing up-to-date technology.
The Honda site preparation quality of rice seedling throwing to rice field has higher requirement, requires the standard that top layer, rice field reaches rotten, flat, clean, shallow.Because the rice seedling got off from unmanned aerial vehicle upthrow is two leaf wholeheartedly or three leaves little rice shoots wholeheartedly, the soil of rice shoot root band sticks together little, shedding the skyborne position of the rice seedling got off from unmanned aerial vehicle is that blade is upper, Tu Tuo under, the degree of depth that Tu Tuo falls into mud only has 1 centimetre ~ 2 cm, because muddy water soaks Tu Tuo after falling into mud, Tu Tuo becomes soft, under suitable temperature conditions, rice shoot root system during soil sticks together stretches out Tu Tuo, extend in mud, the leaf elongation of the rice seedling at Tu Tuo top also launches, within about ten days after rice transplanting, just can grow up to four leaf wholeheartedly or five leaves larger rice seedling wholeheartedly, the seedlings of cereal crops in rice field will present a slice green.Rice transplanting all has certain requirement to nursery, whole, density of seedling broadcasting, rice transplanting time, also has requirement, select the weather rice transplanting without strong wind to meteorological conditions.The unsuitable rice transplanting when heavy rain or wind-force more than 4 grades weather.
After rice seedling throwing, keep face, field melon skin water, within 7 ~ 10 days, for taking root vertical seedling stage, spraying feud agricultural chemicals after vertical seedling, then carrying out normal rice field management.During due to artificial rice transplanting, the footprint that a line another row rice transplanting personnel walk in paddy field will be left in field, during mechanical rice casting, the rat that the road wheel that will leave rice-seedling throwing machine in field travels in paddy field, and shed rice seedling in the low latitude of unmanned aerial vehicle on rice field when flying over paddy field, trace can not be left in paddy field, rice seedling is made to distribute more even in paddy field, be conducive to ventilation and penetrating light between the rice shoot in rice terrace, growing way is balanced, increase yield.
Li Bao town, Nantong City Haian County has established agriculture ministerial level rice seedling throwing ten thousand mu of good quality and high output demonstration areas that area reaches 15772 mu, wherein comprise 3 thousand mu demonstration sheets, 10 hundred mu of demonstration sides, relate to 6 villages such as garden pier, Yang Zhuan, Bao He, fourth institute, Lee's stove, ATrend, 128 villager group, 9505 peasant households.Afternoon on October 24th, 2009, China well-known rice does expert, the National People's Congress of Jiangsu Province former deputy director's Ling Qihong professor leads National agricultural portion, the agricultural Room, Jiangsu Province, Agricultural University Of Nanjing, Yangzhou University paddy rice expert to firsthand investigation, after investigating, paddy rice brainstrust unanimously thinks Haian County's rice seedling throwing advanced technology, rice transplanting Precise and quantitative cultivation, technology arrival rate is high, seedling-throwing technology is not only in first-class level in the whole nation, and also maintains the leading position in the whole world.The average paid paddy per unit area yield more than 700 kilograms through onsite acceptance demonstration area, the highest field per unit area yield 884 kilograms, amount of increase in production reaches 28.9%.The success of large area rice seedling throwing, has liberated a large amount of rural laborers, has significantly improved the efficiency of Rice Production.If adopt solar pilotless plane to shed rice seedling, produce consolidating Estimation of Paddy In Jiangsu Province rice transplanting further in global leading position, unmanned plane research institute of Nanjing Aero-Space University has the technical force and enough means that research and develop civilian unmanned plane.The emerging paddy rice producing region in Northeast Area of China Heilongjiang Province and Jilin Province is scarcely populated, and the time of infertility of this area's rice varieties is short, more needs to adopt solar pilotless plane to shed rice seedling and completes a part of Rice Cropping operation in time.Some paddy rice producing region of Asia, Africa and America is also applicable to using special solar pilotless plane to shed rice seedling.
In order to solve the problems of the technologies described above, the present invention is achieved by the following technical solutions:
By solar pilotless plane 1, fuselage 2, starboard wing 3, port wing 4, starboard tailplane 5, port tailplane 6, yaw rudder 7, solar cell 1, controller 1, conductor wire 10, right photovoltaic self-control switch 11, electrical motor 12, power take-off shaft 13, two bladed propeller 14, front walking wheel 15, controller 2 16, solar cell 2 17, left photovoltaic self-control switch 18, energy-storage battery 1, rice shoot deposits cabin 20, rear walking wheel 21, rice shoot sheds cabin 22, computer-controlled electrical motor 24, shed rice shoot runner 25, shed rice shoot outlet 26, conflux autocontrol switch 27, solar cell 3 28, energy-storage battery 2 29, controller 3 30, solar cell 4 31, energy-storage battery 3 32, controller 4 33 forms the solar pilotless plane shedding rice seedling in a kind of low latitude on rice field jointly, deposit cabin 20 and rice shoot at rice shoot to shed in cabin 22 and have rice shoot 23,
The starboard wing 3 of the front portion of solar pilotless plane 1 is provided with solar cell 1, controller 1, conductor wire 10, right photovoltaic self-control switch 11, the port wing 4 of the front portion of solar pilotless plane 1 is provided with solar cell 2 17, controller 2 16, conductor wire 10, left photovoltaic self-control switch 18, installs electrical motor 12 in the front portion of fuselage 2, power take-off shaft 13, two bladed propeller 14, front walking wheel 15, energy-storage battery 1 and starboard wing 3 and port wing 4, install rice shoot and deposit cabin 20 at the middle part of fuselage 2, rear walking wheel 21, rice shoot sheds cabin 22, computer-controlled electrical motor 24, shed rice shoot runner 25, shed rice shoot outlet 26, at the rear portion of fuselage 2, starboard tailplane 5 is installed, port tailplane 6, yaw rudder 7, conflux autocontrol switch 27, and starboard tailplane 5 is provided with solar cell 3 28, controller 3 30, energy-storage battery 2 29, port tailplane 6 is provided with solar cell 4 31, controller 4 33, energy-storage battery 3 32, is provided with yaw rudder 7 in the centre at the rear portion of fuselage 2, before yaw rudder 7, install the autocontrol switch 27 that confluxes,
Solar cell 1 is connected with controller 1 by conductor wire 10, controller 1 is connected with right photovoltaic self-control switch 11 by conductor wire 10, right photovoltaic self-control switch 11 is connected with energy-storage battery 1 by conductor wire 10, controller 1 is connected with electrical motor 12 by conductor wire 10, solar cell 2 17 is connected with controller 2 16 by conductor wire 10, controller 2 16 is connected with left photovoltaic self-control switch 18 by conductor wire 10, left photovoltaic self-control switch 18 is connected with energy-storage battery 1 by conductor wire 10, controller 2 16 is connected with electrical motor 12 by conductor wire 10, electrical motor 12 is connected with two bladed propeller 14 by power take-off shaft 13, solar cell 3 28 is connected with controller 3 30 by conductor wire 10, controller 3 30 is connected with energy-storage battery 2 29 by conductor wire 10, controller 3 30 is connected with the autocontrol switch 27 that confluxes by conductor wire 10, solar cell 4 31 is connected with controller 4 33 by conductor wire 10, controller 4 33 is connected with energy-storage battery 3 32 by conductor wire 10, controller 4 33 is connected with the autocontrol switch 27 that confluxes by conductor wire 10, the autocontrol switch 27 that confluxes is connected with computer-controlled electrical motor 24 by conductor wire 10.
Solar cell 1, solar cell 2 17, solar cell 3 28 and solar cell 4 31 are crystal silicon solar energy battery or non-crystal silicon solar cell or compound solar cell.
Compared with prior art, the invention has the beneficial effects as follows: 1. solar pilotless plane does not discharge carbon dioxide, sulphur dioxide and deleterious particle thing in the process of flight, is conducive to preserving the ecological environment.2. be equipped with computer-controlled electrical motor in solar pilotless plane, can throw and to transplant seedlings seedling by accurate quantification, make the distribution of rice seedling in rice field more evenly, more reasonable, be conducive to the high yield of paddy rice, stable yields.3. the speed shedding rice seedling is fast, quality good, is conducive to catching farming season, increasing rice yield.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention.
Detailed description of the invention
Rice seedling throwing has and reduces labor intensity, and saving of labor, province rice seedling bed, economizes kind, water-saving, the advantage increasing production, increase income, has more that speed is fast, the measured feature of matter with unmanned aerial vehicle rice transplanting.Solar light irradiation to be arranged on starboard wing and solar cell generation current on port wing, electric current is by conductor wire, controller input electrical motor, in electrical motor, electric energy converts mechanical energy to, and electrical motor consumes mechanical energy to be ordered about power take-off shaft and two bladed propeller fast rotational, make unmanned aerial vehicle produce flying power.Solar cell generation current on solar light irradiation starboard tailplane and on port tailplane, electric current inputs computer-controlled electrical motor by conductor wire, controller and the autocontrol switch that confluxes, computer-controlled electrical motor is driven according to program and sheds the rotation of rice shoot runner, rice shoot is thrown to the rice field of suitable rice transplanting from shedding rice shoot outlet.
Embodiment in is by reference to the accompanying drawings further described by the present invention below:
By solar pilotless plane 1, fuselage 2, starboard wing 3, port wing 4, starboard tailplane 5, port tailplane 6, yaw rudder 7, solar cell 1, controller 1, conductor wire 10, right photovoltaic self-control switch 11, electrical motor 12, power take-off shaft 13, two bladed propeller 14, front walking wheel 15, controller 2 16, solar cell 2 17, left photovoltaic self-control switch 18, energy-storage battery 1, rice shoot deposits cabin 20, rear walking wheel 21, rice shoot sheds cabin 22, computer-controlled electrical motor 24, shed rice shoot runner 25, shed rice shoot outlet 26, conflux autocontrol switch 27, solar cell 3 28, energy-storage battery 2 29, controller 3 30, solar cell 4 31, energy-storage battery 3 32, controller 4 33 forms the solar pilotless plane shedding rice seedling in a kind of low latitude on rice field jointly, deposit cabin 20 and rice shoot at rice shoot to shed in cabin 22 and have rice shoot 23,
The starboard wing 3 of the front portion of solar pilotless plane 1 is provided with solar cell 1, controller 1, conductor wire 10, right photovoltaic self-control switch 11, the port wing 4 of the front portion of solar pilotless plane 1 is provided with solar cell 2 17, controller 2 16, conductor wire 10, left photovoltaic self-control switch 18, installs electrical motor 12 in the front portion of fuselage 2, power take-off shaft 13, two bladed propeller 14, front walking wheel 15, energy-storage battery 1 and starboard wing 3 and port wing 4, install rice shoot and deposit cabin 20 at the middle part of fuselage 2, rear walking wheel 21, rice shoot sheds cabin 22, computer-controlled electrical motor 24, shed rice shoot runner 25, shed rice shoot outlet 26, at the rear portion of fuselage 2, starboard tailplane 5 is installed, port tailplane 6, yaw rudder 7, conflux autocontrol switch 27, and starboard tailplane 5 is provided with solar cell 3 28, controller 3 30, energy-storage battery 2 29, port tailplane 6 is provided with solar cell 4 31, controller 4 33, energy-storage battery 3 32, is provided with yaw rudder 7 in the centre at the rear portion of fuselage 2, before yaw rudder 7, install the autocontrol switch 27 that confluxes,
Solar cell 1 is connected with controller 1 by conductor wire 10, controller 1 is connected with right photovoltaic self-control switch 11 by conductor wire 10, right photovoltaic self-control switch 11 is connected with energy-storage battery 1 by conductor wire 10, controller 1 is connected with electrical motor 12 by conductor wire 10, solar cell 2 17 is connected with controller 2 16 by conductor wire 10, controller 2 16 is connected with left photovoltaic self-control switch 18 by conductor wire 10, left photovoltaic self-control switch 18 is connected with energy-storage battery 1 by conductor wire 10, controller 2 16 is connected with electrical motor 12 by conductor wire 10, electrical motor 12 is connected with two bladed propeller 14 by power take-off shaft 13, solar cell 3 28 is connected with controller 3 30 by conductor wire 10, controller 3 30 is connected with energy-storage battery 2 29 by conductor wire 10, controller 3 30 is connected with the autocontrol switch 27 that confluxes by conductor wire 10, solar cell 4 31 is connected with controller 4 33 by conductor wire 10, controller 4 33 is connected with energy-storage battery 3 32 by conductor wire 10, controller 4 33 is connected with the autocontrol switch 27 that confluxes by conductor wire 10, the autocontrol switch 27 that confluxes is connected with computer-controlled electrical motor 24 by conductor wire 10.
Solar cell 1, solar cell 2 17, solar cell 3 28 and solar cell 4 31 are crystal silicon solar energy battery or non-crystal silicon solar cell or compound solar cell.
Solar light irradiation is arranged on solar cell one generation current on starboard wing, and electric current inputs electrical motor by conductor wire, controller one, and the electric current exported from controller one also can be stored by conductor wire, right photovoltaic self-control switch input energy-storage battery one.Solar light irradiation is arranged on solar cell two generation current on port wing, and electric current inputs electrical motor by conductor wire, controller two, and the electric current exported from controller two also can be stored by conductor wire, left photovoltaic self-control switch input energy-storage battery one.Fine day, right photovoltaic self-control switch closes, and the electric current exported from solar cell one inputs electrical motor by conductor wire, controller one, provides the power source needed for the rotation of power take-off shaft drive double leaf propeller of electrical motor.Fine day, left photovoltaic self-control switch closes, and the electric current exported from solar cell two inputs electrical motor by conductor wire, controller two, provides the power source needed for the rotation of power take-off shaft drive two bladed propeller of electrical motor.At the cloudy day, right photovoltaic self-control switch is opened, and the electric current exported from energy-storage battery one inputs electrical motor by conductor wire, right photovoltaic self-control switch, controller one, provides the power source needed for the rotation of power take-off shaft drive two bladed propeller of electrical motor.At the cloudy day, left photovoltaic self-control switch is opened, and the electric current exported from energy-storage battery one inputs electrical motor by conductor wire, left photovoltaic self-control switch, controller two, provides the power source needed for the rotation of power take-off shaft drive two bladed propeller of electrical motor.Electric energy becomes mechanical energy in electrical motor internal conversion, and electrical motor consumes mechanical energy makes power take-off shaft drive two bladed propeller fast rotational, makes solar pilotless plane produce flying power.Deposit cabin and rice shoot at the rice shoot of the waist of solar pilotless plane to shed in cabin and store the orderly rice shoot etc. of discharge and be ready to use in and shed.Solar light irradiation is arranged on solar cell three generation current on the starboard tailplane at the rear portion of solar pilotless plane, electric current passes through conductor wire, controller three and the autocontrol switch that confluxes input computer-controlled electrical motor, the electric current exported from controller three also can input energy-storage battery two storage by conductor wire, solar light irradiation is arranged on solar cell four generation current on the port tailplane at the rear portion of solar pilotless plane, electric current passes through conductor wire, controller four and the autocontrol switch that confluxes input computer-controlled electrical motor, the electric current exported from controller four also can input energy-storage battery three storage by conductor wire.The autocontrol switch that confluxes can converge electric current, again can auto-control by the magnitude of current of switch.From the electric current that solar cell three and energy-storage battery two export, pass through conductor wire, controller three input is confluxed autocontrol switch, from the electric current that solar cell four and energy-storage battery three export, pass through conductor wire, controller four input is confluxed autocontrol switch, two strands of electric currents are after confluxing and converging in autocontrol switch, then computer-controlled electrical motor is inputted by conductor wire, in computer-controlled electrical motor, electric energy converts mechanical energy to, electrical motor is shed rice shoot runner according to program drive and is rotated according to certain speed, rice shoot is moved fall into and shed rice shoot outlet, drop in low latitude by shedding rice shoot outlet, present blade upper, root and Tu Tuo under state, Tu Tuo continues landing, be absorbed in the degree of depth of top layer, rice field mud 1 centimetre ~ 2 cm, surface and carry out photosynthesis and gas exchanges in the top of blade, the melon skin water soaking Tu Tuo on top layer, rice field becomes soft, the root system of rice shoot stretches out Tu Tuo, penetrate arable layer, the blade of rice shoot grows tall length and width, blade quantity increases, blade area increases, solar pilotless plane is shed rice seedling and is obtained successfully.The calculating function controlling electrical motor regulates and controls flying height and the flying speed of solar pilotless plane, to guarantee the quality shedding rice seedling simultaneously.
Now enumerate embodiment as follows:
Embodiment one:
Rice seedling throwing has and reduces labor intensity, and saving of labor, province rice seedling bed, economizes kind, water-saving, the advantage increasing production, increase income, has more that speed is fast, the measured feature of matter with unmanned aerial vehicle rice transplanting.Solar light irradiation to be arranged on solar pilotless plane starboard wing and crystal silicon solar energy battery generation current on port wing, electric current is by conductor wire, controller input electrical motor, in electrical motor, electric energy converts mechanical energy to, and electrical motor consumes mechanical energy to be ordered about power take-off shaft and two bladed propeller fast rotational, make unmanned aerial vehicle produce flying power.Crystal silicon solar energy battery generation current on solar light irradiation solar pilotless plane starboard tailplane and on port tailplane, electric current inputs computer-controlled electrical motor by conductor wire, controller and the autocontrol switch that confluxes, computer-controlled electrical motor is driven according to program and sheds the rotation of rice shoot runner, rice shoot is thrown to the rice field of suitable rice transplanting from shedding rice shoot outlet.
Embodiment two:
Rice seedling throwing has and reduces labor intensity, and saving of labor, province rice seedling bed, economizes kind, water-saving, the advantage increasing production, increase income, has more that speed is fast, the measured feature of matter with unmanned aerial vehicle rice transplanting.Solar light irradiation to be arranged on solar pilotless plane starboard wing and non-crystal silicon solar cell generation current on port wing, electric current is by conductor wire, controller input electrical motor, in electrical motor, electric energy converts mechanical energy to, and electrical motor consumes mechanical energy to be ordered about power take-off shaft and two bladed propeller fast rotational, make unmanned aerial vehicle produce flying power.Non-crystal silicon solar cell generation current on solar light irradiation solar pilotless plane starboard tailplane and on port tailplane, electric current inputs computer-controlled electrical motor by conductor wire, controller and the autocontrol switch that confluxes, computer-controlled electrical motor is driven according to program and sheds the rotation of rice shoot runner, rice shoot is thrown to the rice field of suitable rice transplanting from shedding rice shoot outlet.
Claims (2)
1. shed a solar pilotless plane for rice seedling in the low latitude on rice field, it is characterized in that, by solar pilotless plane (1), fuselage (2), starboard wing (3), port wing (4), starboard tailplane (5), port tailplane (6), yaw rudder (7), solar cell one (8), controller one (9), conductor wire (10), right photovoltaic self-control switch (11), electrical motor (12), power take-off shaft (13), two bladed propeller (14), front walking wheel (15), controller two (16), solar cell two (17), left photovoltaic self-control switch (18), energy-storage battery one (19), rice shoot deposits cabin (20), rear walking wheel (21), rice shoot sheds cabin (22), computer-controlled electrical motor (24), shed rice shoot runner (25), shed rice shoot outlet (26), conflux autocontrol switch (27), solar cell three (28), energy-storage battery two (29), controller three (30), solar cell four (31), energy-storage battery three (32), the solar pilotless plane of rice seedling jointly shed in a kind of low latitude on rice field of composition by controller four (33), deposits cabin (20) and rice shoot shed in cabin (22) and have rice shoot (23) at rice shoot,
The starboard wing (3) of the front portion of solar pilotless plane (1) is provided with solar cell one (8), controller one (9), conductor wire (10), right photovoltaic self-control switch (11), the port wing (4) of the front portion of solar pilotless plane (1) is provided with solar cell two (17), controller two (16), conductor wire (10), left photovoltaic self-control switch (18), installs electrical motor (12) in the front portion of fuselage (2), power take-off shaft (13), two bladed propeller (14), front walking wheel (15), energy-storage battery one (19) and starboard wing (3) and port wing (4), install rice shoot and deposit cabin (20) at the middle part of fuselage (2), rear walking wheel (21), rice shoot sheds cabin (22), computer-controlled electrical motor (24), shed rice shoot runner (25), shed rice shoot outlet (26), at the rear portion of fuselage (2), starboard tailplane (5) is installed, port tailplane (6), yaw rudder (7), conflux autocontrol switch (27), and starboard tailplane (5) is provided with solar cell three (28), controller three (30), energy-storage battery two (29), port tailplane (6) is provided with solar cell four (31), controller four (33), energy-storage battery three (32), is provided with yaw rudder (7) in the centre at the rear portion of fuselage (2), before yaw rudder (7), install the autocontrol switch (27) that confluxes,
Solar cell one (8) is connected with controller one (9) by conductor wire (10), controller one (9) is connected with right photovoltaic self-control switch (11) by conductor wire (10), right photovoltaic self-control switch (11) is connected with energy-storage battery one (19) by conductor wire (10), controller one (9) is connected with electrical motor (12) by conductor wire (10), solar cell two (17) is connected with controller two (16) by conductor wire (10), controller two (16) is connected with left photovoltaic self-control switch (18) by conductor wire (10), left photovoltaic self-control switch (18) is connected with energy-storage battery one (19) by conductor wire (10), controller two (16) is connected with electrical motor (12) by conductor wire (10), electrical motor (12) is connected with two bladed propeller (14) by power take-off shaft (13), solar cell three (28) is connected with controller three (30) by conductor wire (10), controller three (30) is connected with energy-storage battery two (29) by conductor wire (10), controller three (30) is connected with the autocontrol switch that confluxes (27) by conductor wire (10), solar cell four (31) is connected with controller four (33) by conductor wire (10), controller four (33) is connected with energy-storage battery three (32) by conductor wire (10), controller four (33) is connected with the autocontrol switch that confluxes (27) by conductor wire (10), the autocontrol switch (27) that confluxes is connected with computer-controlled electrical motor (24) by conductor wire (10).
2. in a kind of low latitude on rice field according to claim 1, shed the solar pilotless plane of rice seedling, it is characterized in that, described solar cell one (8), solar cell two (17), solar cell three (28) and solar cell four (31) are crystal silicon solar energy battery or non-crystal silicon solar cell or compound solar cell.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310621233.9A CN103612757B (en) | 2013-11-29 | 2013-11-29 | The solar pilotless plane of rice seedling is shed in a kind of low latitude on rice field |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310621233.9A CN103612757B (en) | 2013-11-29 | 2013-11-29 | The solar pilotless plane of rice seedling is shed in a kind of low latitude on rice field |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103612757A CN103612757A (en) | 2014-03-05 |
| CN103612757B true CN103612757B (en) | 2015-09-30 |
Family
ID=50163486
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310621233.9A Active CN103612757B (en) | 2013-11-29 | 2013-11-29 | The solar pilotless plane of rice seedling is shed in a kind of low latitude on rice field |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103612757B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109275395A (en) * | 2017-07-21 | 2019-01-29 | 江苏年豊现代农业科技有限公司 | The identification of machine transplanting of rice rice shoot burst and method of filling the gaps with seedlings |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101963806A (en) * | 2010-10-15 | 2011-02-02 | 农业部南京农业机械化研究所 | Unmanned helicopter pesticide applying operation automatic control system and method based on GPS (Global Positioning System) navigation |
| CN102897323A (en) * | 2012-10-31 | 2013-01-30 | 无锡同春新能源科技有限公司 | Unmanned spraying and fighting aircraft for mosquito killing |
| CN102960104A (en) * | 2012-11-13 | 2013-03-13 | 上海交通大学无锡研究院 | Unmanned rice seedling slinging machine |
| CN202842053U (en) * | 2012-09-11 | 2013-04-03 | 陈博 | Unmanned helicopter for seed production and pollination of rice |
| CN203558207U (en) * | 2013-11-29 | 2014-04-23 | 无锡同春新能源科技有限公司 | Solar unmanned airplane for throwing rice seedlings in sky above rice fields |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20030130767A1 (en) * | 2002-01-07 | 2003-07-10 | Carroll Ernest A. | Method of and apparatus for acquiring aerial imagery for precision farming |
| JP4140004B2 (en) * | 2003-02-21 | 2008-08-27 | ヤマハ発動機株式会社 | Unmanned helicopter |
| KR20110104405A (en) * | 2010-03-16 | 2011-09-22 | 동국대학교 산학협력단 | Hybrid power-supplying apparatus for unmanned helicopter |
-
2013
- 2013-11-29 CN CN201310621233.9A patent/CN103612757B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101963806A (en) * | 2010-10-15 | 2011-02-02 | 农业部南京农业机械化研究所 | Unmanned helicopter pesticide applying operation automatic control system and method based on GPS (Global Positioning System) navigation |
| CN202842053U (en) * | 2012-09-11 | 2013-04-03 | 陈博 | Unmanned helicopter for seed production and pollination of rice |
| CN102897323A (en) * | 2012-10-31 | 2013-01-30 | 无锡同春新能源科技有限公司 | Unmanned spraying and fighting aircraft for mosquito killing |
| CN102960104A (en) * | 2012-11-13 | 2013-03-13 | 上海交通大学无锡研究院 | Unmanned rice seedling slinging machine |
| CN203558207U (en) * | 2013-11-29 | 2014-04-23 | 无锡同春新能源科技有限公司 | Solar unmanned airplane for throwing rice seedlings in sky above rice fields |
Non-Patent Citations (1)
| Title |
|---|
| 《无人机喷洒技术的研究》;吴小伟等;《农机化研究》;20100731(第7期);第224-228页 * |
Also Published As
| Publication number | Publication date |
|---|---|
| CN103612757A (en) | 2014-03-05 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN201640082U (en) | Intelligent multi-storey factory seedling raising device for sunlight greenhouse | |
| CN206791172U (en) | It is a kind of can subregion adjustment shading solar greenhouse | |
| CN104641887B (en) | Ground type photovoltaic base under a kind of Desert Conditions | |
| CN101238783A (en) | Method and device for automatically regulating sunlight strength and promoting vegetation | |
| CN106718558A (en) | One elite stand light one Chinese gooseberry garden and Kiwi berry implantation methods | |
| CN101278647A (en) | Device for cultivating forestry seedling with complementary applications of solar photovoltaic power and wind power | |
| CN103612759A (en) | Solar unmanned airplane used for direct rice seeding from low altitudes above rice field | |
| CN104472335A (en) | Greenhouse type plant factory system for flower production | |
| CN102948346A (en) | Solar photovoltaic greenhouse for cultivating fig | |
| CN203558207U (en) | Solar unmanned airplane for throwing rice seedlings in sky above rice fields | |
| CN201238520Y (en) | Device for cultivating forestry seedling with complementary applications of solar photovoltaic power and wind power | |
| CN205249949U (en) | Tracking formula photovoltaic green house system | |
| CN103612757B (en) | The solar pilotless plane of rice seedling is shed in a kind of low latitude on rice field | |
| CN103843551A (en) | Desert management method and setting | |
| CN206165310U (en) | Seedling growing greenhouse system | |
| CN203302070U (en) | Tree breeding shed | |
| CN102972234A (en) | Solar photovoltaic greenhouse for mulberry planting | |
| CN103461052B (en) | Technology for growing bananas on hillsides | |
| Nelkin et al. | Sustainable controlled environment agriculture for urban areas | |
| CN107371959A (en) | The monkey peach orchard that a kind of and photovoltaic plant combines is divulged information, windproof and antifreeze method | |
| CN101632339A (en) | Flower forcing device of solar energy photovoltaic power generation system in peony plant | |
| CN203558209U (en) | Solar unmanned airplane for directly sowing rice seeds in sky above rice fields | |
| CN201045808Y (en) | An apparatus for governing desert | |
| CN206423288U (en) | A kind of device for fetching water | |
| CN204047369U (en) | A kind of high and cold energy saving greenhouse |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |