CN110979684A - Can realize unmanned aerial vehicle of accurate seeding - Google Patents
Can realize unmanned aerial vehicle of accurate seeding Download PDFInfo
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- CN110979684A CN110979684A CN201911267511.9A CN201911267511A CN110979684A CN 110979684 A CN110979684 A CN 110979684A CN 201911267511 A CN201911267511 A CN 201911267511A CN 110979684 A CN110979684 A CN 110979684A
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- 238000010899 nucleation Methods 0.000 title claims abstract description 15
- 230000000087 stabilizing effect Effects 0.000 claims description 42
- 238000002485 combustion reaction Methods 0.000 claims description 21
- 239000012528 membrane Substances 0.000 claims description 19
- 239000001273 butane Substances 0.000 claims description 11
- 238000009434 installation Methods 0.000 claims description 11
- IJDNQMDRQITEOD-UHFFFAOYSA-N n-butane Chemical group CCCC IJDNQMDRQITEOD-UHFFFAOYSA-N 0.000 claims description 10
- OFBQJSOFQDEBGM-UHFFFAOYSA-N n-pentane Natural products CCCCC OFBQJSOFQDEBGM-UHFFFAOYSA-N 0.000 claims description 10
- 238000009331 sowing Methods 0.000 abstract description 22
- 230000005540 biological transmission Effects 0.000 abstract description 4
- 238000012803 optimization experiment Methods 0.000 abstract description 2
- 239000007789 gas Substances 0.000 description 80
- 229910001369 Brass Inorganic materials 0.000 description 7
- 239000010951 brass Substances 0.000 description 7
- 239000002737 fuel gas Substances 0.000 description 5
- 230000009471 action Effects 0.000 description 4
- 238000004880 explosion Methods 0.000 description 4
- 239000000446 fuel Substances 0.000 description 4
- 229910000838 Al alloy Inorganic materials 0.000 description 3
- 239000007788 liquid Substances 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 239000011268 mixed slurry Substances 0.000 description 3
- 230000001105 regulatory effect Effects 0.000 description 3
- 238000007789 sealing Methods 0.000 description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 229910000589 SAE 304 stainless steel Inorganic materials 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000002803 fossil fuel Substances 0.000 description 1
- 239000002828 fuel tank Substances 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000002689 soil Substances 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
Images
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/16—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Sowing (AREA)
Abstract
The invention discloses an unmanned aerial vehicle capable of realizing accurate sowing, wherein a controller, a seed pushing device and a seed launching device are installed on an unmanned aerial vehicle body, the seed pushing device comprises a seed bin, a first motor, a rotating shaft and a rotating wheel, the first motor rotates to drive the rotating shaft to rotate, the rotating shaft drives the rotating wheel to rotate, at least three transport bins are uniformly distributed on the rotating wheel, an inclined transport pipe is arranged below the rotating wheel, a seed inlet is formed in the end part of the transport pipe, a vertical baffle is installed at the seed inlet, a counter is installed in the transport pipe, the counter is connected with the controller, and the controller is in signal connection with the first motor. The average transmitting frequency of the sowing unmanned aerial vehicle prototype measured by the invention can reach one transmission per 0.7 second, and when the optimization experiment is carried out in the later period, the transmitting frequency is predicted to reach the frequency of 3 transmissions per second. If on a land, when utilizing this seeding unmanned aerial vehicle of many shelves to sow to a land, can improve seeding speed by a bigger degree.
Description
Technical Field
The invention relates to an unmanned aerial vehicle capable of realizing accurate seeding, and belongs to the field of agricultural unmanned aerial vehicles.
Background
Plant protection unmanned aerial vehicle is the unmanned aircraft who is used for agriculture and forestry plant protection operation, and this kind of unmanned aerial vehicle mostly flies to control, sprays or sowing mechanism triplex by flight platform, navigation, and the operation of spraying is realized flying to control through the remote control on accessible ground or navigation, and current unmanned aerial vehicle seeding is set up seed case on unmanned aerial vehicle more, and the in-process of flying is sowed through the switching of seed case. The existing modes are broadcast sowing, and in the sowing process of certain crops, dibbling is required to be used, so that research on a dibbling unmanned aerial vehicle is urgent.
Disclosure of Invention
The purpose of the invention is as follows: in order to overcome the defects in the prior art, the invention provides the unmanned aerial vehicle capable of realizing accurate sowing, and the seeds can be injected into soil through the seed launching device so as to realize the purpose of deeply sowing crops.
The technical scheme is as follows: in order to solve the technical problems, the unmanned aerial vehicle capable of realizing accurate sowing comprises an unmanned aerial vehicle body, wherein a controller, a seed pushing device and a seed launching device are installed on the unmanned aerial vehicle body, the seed pushing device comprises a seed bin, a first motor, a rotating shaft and a rotating wheel, the first motor rotates to drive the rotating shaft to rotate, the rotating shaft drives the rotating wheel to rotate, at least three conveying bins are uniformly distributed on the rotating wheel, arc-shaped baffles are installed on two sides of the rotating wheel and fixedly connected with the seed bin through a support, an inclined conveying pipe is arranged below the rotating wheel, a seed inlet is formed in the end part of the conveying pipe, a vertical baffle is installed at the seed inlet, a counter is installed in the conveying pipe and connected with the controller, and the controller is in signal connection with the first motor; seed emitter contains gas jar, blender, vacuum pump, combustion chamber and launching tube, the gas of gas jar gets into the blender and mixes the back, sends into the combustion chamber through the vacuum pump, ignites through ignition switch in the combustion chamber, produces high-pressure gas, and high-pressure gas enters into in the launching tube, launching tube and transportation pipe intercommunication, and the seed in the transportation pipe enters into the launching tube, jets into earth with the seed through high-pressure gas in, realizes the purpose of dibbling.
Preferably, the mixer comprises a mixer body and a pressure stabilizing chamber, a gas inlet and an air inlet are respectively arranged at two ends of the mixer body, the gas inlet is communicated with the pressure stabilizing chamber inlet, an electromagnetic valve is arranged at the pressure stabilizing chamber inlet, an electromagnetic valve reset spring is arranged at the bottom of the electromagnetic valve, an electromagnetic valve coil is sleeved outside the electromagnetic valve, and the electromagnetic valve coil controls the electromagnetic valve to move up and down; a lever seat is installed in the pressure stabilizing valve, a lever plug is connected to one end of the lever on the lever seat and is positioned at the inlet of the pressure stabilizing chamber, the other end of the lever is connected with a connecting rod, the connecting rod is connected with a pressure membrane, a pressure stabilizing chamber cover is installed above the pressure membrane, a pressure membrane reset spring is installed between the pressure membrane and the pressure stabilizing chamber cover, and the pressure membrane and the pressure stabilizing chamber cover are fixedly installed on the mixer body; the outlet of the pressure stabilizing chamber is communicated with an air inlet through a gas pipe, the air inlet is communicated with a gas-air mixing chamber, a rotating shaft is arranged in the gas-air mixing chamber, a mixing paddle is arranged on the rotating shaft, a mixed gas outlet is arranged in the gas-air mixing chamber, and the uniformly mixed gas is discharged through the mixed gas outlet.
Preferably, a gas fine-adjustment valve for adjusting the flow rate is arranged on the gas pipe.
Preferably, the launching tube is a foldable part and comprises a straight tube and a foldable tube, one end of the straight tube is connected with one end of a three-way valve, the second end of the three-way valve is connected with the combustion chamber, and the third end of the three-way valve is connected with the seed conveying device; the folding pipe is installed on the installation seat, the installation seat is hinged to the straight pipe, the installation seat is provided with a connection seat, and the connection seat is connected with the folding device.
Preferably, the folding device comprises a shell, two pairs of bearings are arranged on the shell, a first worm gear rod and a second worm gear rod are respectively sleeved on the two pairs of bearings, worm gears which are meshed with each other are arranged in the middle of the first worm gear rod and the second worm gear rod, a threaded through hole is formed in the center of the first worm, a threaded sliding rod is arranged in the threaded through hole, the end part of the sliding rod is connected with the connecting seat, one end of the second worm gear rod is connected with a lifting motor, and the lifting motor is connected with the controller; the second worm gear rod is driven to rotate through the lifting motor, the second worm gear rod drives the first worm gear rod to rotate, the first worm gear rod rotates, the sliding rod is driven to move up and down through threads, and therefore the launching tube is driven to be folded.
Preferably, the gas in the fuel tank is butane.
Preferably, the conveying pipe is provided with a photoelectric counter which is in signal connection with a controller, and the controller is in signal connection with the high-pressure ignition head.
The invention uses butane fuel as power, and utilizes the air pressure generated by explosion of air-fuel mixture in a sealed space to launch seeds. The energy density of butane gas is larger than that of compressed air, the problem of short endurance of the compressed air can be solved, and seeds can be shot into the ground by high-pressure gas generated by explosion to a depth of dozens of centimeters. The high-pressure gas generated by the explosion of butane fuel in a limited closed space is used for emitting seeds, and the cruising ability of the sowing system is improved by utilizing the characteristic of high energy density of butane gas. The kinetic energy emitted by each seed is provided by the energy generated by each explosion in the combustion chamber, so that the seeds can be shot into the ground to a certain depth, and the problem of deep sowing is solved.
The use of butane as a power source can greatly reduce carbon emissions for the following reasons; when the compressed air is prepared, firstly, the energy of fossil fuel is converted into mechanical energy by using an internal combustion engine, then the mechanical energy is converted into the internal energy of the compressed air, and when the seeds are launched, the energy of the compressed air is converted into the kinetic energy of the seeds. And the butane is directly used as fuel to launch the seeds, so that the energy loss in the process can be avoided, the utilization efficiency of the energy is improved, and the carbon emission is greatly reduced.
In the present invention, the mixer main body is cast from an aluminum alloy; the gas fine-tuning valve is made of brass, and the size of a channel of a gas outlet of mixed gas can be changed by rotating the valve body, so that the flow can be adjusted; the mixed slurry is made of brass and can rotate under the impact of airflow, so that the mixed gas forms vortex in the gas-air mixing chamber, and the aim of uniformly mixing the gas is fulfilled; the outer surface of the mixed gas outlet is provided with anti-slip lines, so that the pipeline can be prevented from slipping; the air inlet is formed by pouring aluminum alloy; the bush is made of brass and is sleeved on the central rotating shaft in the air-gas mixing chamber with the mixed slurry, so that two adjacent mixed slurries do not influence each other during working; the plug valve is made of brass and is used for adjusting the amount of fuel gas entering the mixing chamber; the electromagnetic valve body is made of 304 steel and driven by the electromagnetic valve, and a rubber sleeve is sleeved at the lower end of the valve body and the air inlet of the pressure stabilizing chamber, so that a good sealing effect can be achieved when the power is off; the outer surface of the gas inlet is provided with anti-skid lines, so that the gas pipe can be prevented from falling off; the electromagnetic valve and the electromagnetic valve cover are made of brass; the valve cover of the plug valve is made of brass; the plug valve is made of brass and has the function of adjusting the gas-air mixing ratio; the pressure stabilizing chamber cover is fixed on the mixer body by four screws; the contact part of the lever plug and the gas inlet is sleeved with a rubber plug, and the rest of the whole body is formed by pouring aluminum alloy.
Under the control of the control system program, when the electromagnetic valve is sucked up by the electromagnetic coil (when the electromagnetic valve is in a power-off state, the upper end of the electromagnetic valve is propped against the inlet of the pressure stabilizing chamber under the action of the electromagnetic valve return spring), high-pressure fuel gas flows into the pressure stabilizing chamber, and when the pressure in the pressure stabilizing chamber reaches a certain value, a pressure film in the pressure stabilizing chamber moves upwards, so that the connecting rod is driven to move upwards. The lower end of the connecting rod is sleeved at the left end of the lever plug, when the connecting rod moves upwards, the right end of the lever plug is lifted, and due to the lever action, the left end of the lever plug moves downwards, so that fuel gas is prevented from entering the pressure stabilizing chamber. When the air pressure in the pressure stabilizing chamber is reduced, the pressure membrane moves downwards under the action of the pressure membrane return spring, so that the air enters the pressure stabilizing chamber again. After the pressure of the gas is regulated in the pressure stabilizing chamber, high-pressure gas can be converted into stable low-pressure gas, and at the moment, the low-pressure gas is discharged from the pressure stabilizing chamber and passes through the plug valve and the plug valve, so that the gas quantity of the gas entering the mixing chamber can be regulated. After being regulated by the plug valve, the fuel gas flows into the air inlet from the fuel gas pipe. When the air pump works, external air passes through the air inlet and is accelerated to high-speed gas at a throat of the air inlet (the flow rate of the gas is increased by using the Bernoulli theorem through a slit in the middle of the throat), and the gas mixed with the gas flowing out of the gas pipe flows into the gas-air mixing chamber. After the gas and the air that flow at a high speed flow into the mixing chamber, can strike the gas mixing thick liquid in the blender for the gas mixing thick liquid is rotatory, and rotatory gas mixing thick liquid can let air and gas form a plurality of vortexes in gas-air mixing chamber, thereby makes air and gas mix more evenly. The mixed gas uniformly mixed in the gas-air mixing chamber flows into a mixed gas outlet under the action of a vacuum pump, is adjusted into gas flow with proper size by a mixed gas fine adjustment valve in a mixed gas outlet pipe, then flows into a vacuum pump, and is delivered to a position needing to be combusted by the vacuum pump.
Has the advantages that: compared with the prior art, the invention has the following advantages:
1. the sowing unmanned aerial vehicle can realize deep sowing of crops, greatly improves the sowing efficiency, and fills the blank of unmanned aerial vehicle sowing at home and abroad in the aspect of deep sowing;
2. in the invention, the measured average transmitting frequency of the model machine of the sowing unmanned aerial vehicle can reach one transmission per 0.7 second, and when the optimization experiment is carried out in the later period, the transmitting frequency is predicted to reach the frequency of 3 transmissions per second. If on a land, when utilizing this seeding unmanned aerial vehicle of many shelves to sow to a land, can improve seeding speed by a bigger degree.
3. The sowing unmanned aerial vehicle can also greatly improve the utilization rate of mountainous lands, and the sowing system is carried on the unmanned aerial vehicle, so that sowing can be carried out on lands with complex terrains or difficult-to-reach lands.
Drawings
FIG. 1 is a schematic structural diagram of the present invention.
Fig. 2 is a flow chart of the combustion chamber air supply system of the sowing unmanned aerial vehicle.
Fig. 3 is a schematic diagram of the mixer structure.
Fig. 4 is a schematic cross-sectional view taken vertically in fig. 3.
Fig. 5 is a schematic cross-sectional view of the air intake horizontal plane.
Fig. 6 is a schematic structural view of the folding device.
In the drawings: 1-high-pressure ignition head, 2-combustion chamber, 3-combustion chamber air inlet pipe, 4-seed bin, 5-transportation bin, 6-arc baffle, 7-rotating wheel, 8-vertical baffle, 9-transportation pipe, 10-emission pipe, 13-butane gas tank, 14-vacuum pump, 31-mixer body, 32-mixed gas fine adjustment valve, 33-mixing paddle, 34-mixed gas outlet, 35-air inlet, 36-lining, 37-plug valve, 38-electromagnetic valve, 39-gas inlet, 310-electromagnetic valve coil, 311-electromagnetic valve reset spring, 312-electromagnetic valve spring fixing cover, 313-plug valve fixing cover, 314-plug valve sealing ring, 315-gas pipe, 316-pressure stabilizing chamber cover, 317-a pressure membrane return spring, 318-a pressure membrane, 319-a connecting rod, 320-a lever plug, 321-a pressure stabilizing chamber, 322-a gas-air mixing chamber, 101 a second worm gear, 102 a lifting motor, 103 a connecting rod, 104 a connecting seat, 105 a straight pipe, 106 a sliding rod, 107 a first worm gear and 108-a mounting plate.
Detailed Description
The present invention will be further described with reference to the accompanying drawings.
As shown in fig. 1 to 6, the unmanned aerial vehicle capable of realizing precise sowing comprises an unmanned aerial vehicle body, wherein a controller, a seed pushing device and a seed launching device are mounted on the unmanned aerial vehicle body, the seed pushing device comprises a seed bin 4, a first motor, a rotating shaft and a rotating wheel 7, the first motor rotates to drive the rotating shaft to rotate, the rotating shaft drives the rotating wheel 7 to rotate, at least three transport bins 5 are uniformly distributed on the rotating wheel 7, circular arc-shaped baffles 6 are mounted on two sides of the rotating wheel 7, the baffles are fixedly connected with the seed bin 4 through a support, an inclined transport pipe 9 is arranged below the rotating wheel 7, a seed inlet is formed in the end of the transport pipe 9, a vertical baffle 8 is mounted at the seed inlet, a counter is mounted in the transport pipe 9 and connected with the controller, and the controller is in signal connection with the first motor; seed emitter contains gas jar 13, blender, vacuum pump 14, combustion chamber 2 and launching tube 10, gas in the gas jar 13 is the butane, gas entering blender of gas jar 13 mixes the back, sends into combustion chamber 2 through vacuum pump 14, ignites through high-pressure ignition head 1 in combustion chamber 2, produces high-pressure gas, and high-pressure gas enters into launching tube 10 in, launching tube 10 and transport pipe 9 intercommunication, and the seed in the transport pipe 9 enters into launching tube 10 in, jets into earth with the seed through high-pressure gas, realizes the purpose of dibble seeding.
In the invention, the mixer comprises a mixer body 31 and a pressure stabilizing chamber 321, a gas inlet and an air inlet 35 are respectively arranged at two ends of the mixer body 31, the gas inlet 39 is communicated with an inlet of the pressure stabilizing chamber 321, an electromagnetic valve 38 is arranged at the inlet of the pressure stabilizing chamber 321, an electromagnetic valve return spring 311 is arranged at the bottom of the electromagnetic valve 38, the electromagnetic valve return spring 311 is arranged in the mixer body through an electromagnetic valve spring fixing cover 312, an electromagnetic valve coil 310 is sleeved outside the electromagnetic valve 38, and the up-and-down movement of the electromagnetic valve 38 is controlled through the electromagnetic valve coil 310; a lever seat is installed in the pressure stabilizing valve, one end of a lever is connected with a lever plug 320 on the lever seat, the lever plug 320 is positioned at the inlet of a pressure stabilizing chamber 321, the other end of the lever is connected with a connecting rod 319, the connecting rod 319 is connected with a pressure membrane 318, a pressure stabilizing chamber cover 316 is installed above the pressure membrane 318, a pressure membrane reset spring 317 is installed between the pressure membrane 318 and the pressure stabilizing chamber cover 316, and the pressure membrane 318 and the pressure stabilizing chamber cover 316 are fixedly installed on the mixer body 31; the outlet of the pressure stabilizing chamber 321 is communicated with an air inlet 35 through a gas pipe 315, the air inlet 35 is communicated with a gas-air mixing chamber 322, a rotating shaft is installed in the gas-air mixing chamber 322, mixing blades 33 are installed on the rotating shaft, adjacent mixing blades 33 are separated through a lining 36, a mixed gas outlet 34 is formed in the gas-air mixing chamber 322, and uniformly mixed gas is discharged through the mixed gas outlet 34 and enters the combustion chamber from a combustion chamber gas inlet pipe 3.
In the present invention, a plug valve 37 is mounted on a gas pipe 315, the plug valve 37 is mounted in the mixer body through a plug valve fixing cover 313 and a plug valve sealing ring 314 to adjust the flow rate of the gas, and a mixed gas fine adjustment valve 32 is provided on a mixed gas outlet 34 to adjust the flow rate of the mixed gas.
In the invention, the launching tube 10 is a foldable part, the launching tube 10 comprises a straight tube 105 and a foldable tube, one end of the straight tube 105 is connected with one end of a three-way valve, the second end of the three-way valve is connected with the combustion chamber 2, and the third end of the three-way valve is connected with a seed conveying device; the folding pipe is arranged on an installation seat, the installation seat is hinged on the straight pipe 105, a connection seat 104 is arranged on the installation seat, and the connection seat 104 is connected with the folding device; the folding device comprises a shell (not shown), the shell is installed on an installation plate, the installation plate is connected with the unmanned aerial vehicle body, two pairs of bearings are arranged on the shell, a first worm gear 107 and a second worm gear 101 are sleeved on the two pairs of bearings respectively, worm gears which are meshed with each other are arranged in the middle of the first worm gear 107 and the second worm gear 101, a threaded through hole is formed in the center of the first worm gear, a threaded slide rod 106 is installed in the threaded through hole, the end part of the slide rod 106 is hinged with a connection seat 104 through a connection rod 103, and one end of the second worm gear 101 is connected with a lifting motor 102; the second worm gear 101 is driven to rotate by the lifting motor 102, the second worm gear 101 drives the first worm gear 107 to rotate, the first worm gear 107 rotates, and the slide bar 106 is driven to move up and down by the screw thread, so that the launching tube 10 is driven to fold.
When the high-pressure gas generator is used, butane enters the pressure stabilizing chamber 321 through the gas inlet, is subjected to pressure regulation through the pressure stabilizing chamber 321, is mixed with air in the gas-air mixing chamber 322, is sent into the combustion chamber 2 through the vacuum pump 14, and is ignited through the high-pressure ignition head 1 in the combustion chamber 2 to generate high-pressure gas; meanwhile, the first motor rotates to drive the rotating wheel to rotate, when the transport bin moves to the lower part, the seeds fall into the transmitting pipe 10, and the high-pressure gas compressed air injects the seeds into the ground to realize deep sowing, so that the purpose of dibbling is realized.
The above description is only of the preferred embodiments of the present invention, and it should be noted that: it will be apparent to those skilled in the art that various modifications and adaptations can be made without departing from the principles of the invention and these are intended to be within the scope of the invention.
Claims (6)
1. The utility model provides an unmanned aerial vehicle that can realize accurate seeding which characterized in that: the seed pushing device comprises a seed bin, a first motor, a rotating shaft and a rotating wheel, wherein the first motor rotates to drive the rotating shaft to rotate, the rotating shaft drives the rotating wheel to rotate, at least three transport bins are uniformly distributed on the rotating wheel, arc-shaped baffles are mounted on two sides of the rotating wheel, the baffles are fixedly connected with the seed bin through a support, an inclined transport pipe is arranged below the rotating wheel, a seed inlet is formed in the end part of the transport pipe, a vertical baffle is mounted at the seed inlet, a counter is mounted in the transport pipe, the counter is connected with the controller, and the controller is in signal connection with the first motor; seed emitter contains gas jar, blender, vacuum pump, combustion chamber and launching tube, the gas of gas jar gets into the blender and mixes the back, sends into the combustion chamber through the vacuum pump, ignites through ignition switch in the combustion chamber, produces high-pressure gas, and high-pressure gas enters into in the launching tube, launching tube and transportation pipe intercommunication, and the seed in the transportation pipe enters into the launching tube, jets into earth with the seed through high-pressure gas in, realizes the purpose of dibbling.
2. The unmanned aerial vehicle capable of realizing precise seeding according to claim 1, wherein: the mixer comprises a mixer body and a pressure stabilizing chamber, wherein a gas inlet and an air inlet are respectively formed in two ends of the mixer body, the gas inlet is communicated with the pressure stabilizing chamber inlet, an electromagnetic valve is arranged at the pressure stabilizing chamber inlet, an electromagnetic valve reset spring is installed at the bottom of the electromagnetic valve, an electromagnetic valve coil is sleeved on the outer side of the electromagnetic valve, and the electromagnetic valve coil controls the electromagnetic valve to move up and down; a lever seat is installed in the pressure stabilizing valve, a lever plug is connected to one end of the lever on the lever seat and is positioned at the inlet of the pressure stabilizing chamber, the other end of the lever is connected with a connecting rod, the connecting rod is connected with a pressure membrane, a pressure stabilizing chamber cover is installed above the pressure membrane, a pressure membrane reset spring is installed between the pressure membrane and the pressure stabilizing chamber cover, and the pressure membrane and the pressure stabilizing chamber cover are fixedly installed on the mixer body; the outlet of the pressure stabilizing chamber is communicated with an air inlet through a gas pipe, the air inlet is communicated with a gas-air mixing chamber, a rotating shaft is arranged in the gas-air mixing chamber, a mixing paddle is arranged on the rotating shaft, a mixed gas outlet is arranged in the gas-air mixing chamber, and the uniformly mixed gas is discharged through the mixed gas outlet.
3. The unmanned aerial vehicle capable of realizing precise seeding according to claim 2, wherein: and a gas fine-adjustment valve for adjusting the flow is arranged on the gas pipe.
4. The unmanned aerial vehicle capable of realizing precise seeding according to claim 1, wherein: the transmitting pipe is a foldable part and comprises a straight pipe and a folding pipe, one end of the straight pipe is connected with one end of a three-way valve, the second end of the three-way valve is connected with the combustion chamber, and the third end of the three-way valve is connected with the seed conveying device; the folding pipe is installed on the installation seat, the installation seat is hinged to the straight pipe, the installation seat is provided with a connection seat, and the connection seat is connected with the folding device.
5. The unmanned aerial vehicle capable of realizing precise seeding according to claim 4, wherein: the folding device comprises a shell, two pairs of bearings are arranged on the shell, a first worm gear rod and a second worm gear rod are sleeved on the two pairs of bearings respectively, worm gears which are meshed with each other are arranged in the middle of the first worm gear rod and the middle of the second worm gear rod, a threaded through hole is formed in the center of the first worm, a threaded sliding rod is installed in the threaded through hole, the end part of the sliding rod is connected with a connecting seat, one end of the second worm gear rod is connected with a lifting motor, and the lifting motor is connected with a controller; the second worm gear rod is driven to rotate by the lifting motor, so that the first worm gear rod is driven to rotate by the second worm gear rod, the slide rod is driven to move up and down by the threads, and the launching tube is driven to be folded.
6. The unmanned aerial vehicle capable of realizing precise seeding according to claim 1, wherein: the gas in the gas tank is butane.
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Cited By (1)
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CN112238943A (en) * | 2020-10-20 | 2021-01-19 | 鲁莺 | Agricultural seeding unmanned aerial vehicle of deviation is prevented in ration input |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2011220471A (en) * | 2010-04-12 | 2011-11-04 | Rinnai Corp | Safety valve |
US20120255536A1 (en) * | 2011-04-08 | 2012-10-11 | David Deng | Heating system |
CN107435926A (en) * | 2017-10-11 | 2017-12-05 | 河南科技大学 | A kind of liquid fuel and Combustion of Premixed device |
CN107750543A (en) * | 2017-11-20 | 2018-03-06 | 中国农业大学 | Unmanned aerial vehicle onboard is precisely to target seeding system and operational method |
CN207093882U (en) * | 2017-07-10 | 2018-03-13 | 张伟 | A kind of safety relief valve |
CN208593497U (en) * | 2018-07-31 | 2019-03-12 | 宁夏翼航智控科技有限公司 | A kind of plant protection drone |
CN109665103A (en) * | 2019-01-14 | 2019-04-23 | 珠海卡特瑞科农林航空装备研究所有限公司 | Seeding apparatus and sowing unmanned plane with the device |
CN208993929U (en) * | 2018-09-30 | 2019-06-18 | 广州极飞科技有限公司 | A kind of material spreading gear and unmanned plane |
KR20190075473A (en) * | 2017-12-21 | 2019-07-01 | 한국해양과학기술원 | Apparatus for direct seeding using drone |
-
2019
- 2019-12-11 CN CN201911267511.9A patent/CN110979684A/en active Pending
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2011220471A (en) * | 2010-04-12 | 2011-11-04 | Rinnai Corp | Safety valve |
US20120255536A1 (en) * | 2011-04-08 | 2012-10-11 | David Deng | Heating system |
CN207093882U (en) * | 2017-07-10 | 2018-03-13 | 张伟 | A kind of safety relief valve |
CN107435926A (en) * | 2017-10-11 | 2017-12-05 | 河南科技大学 | A kind of liquid fuel and Combustion of Premixed device |
CN107750543A (en) * | 2017-11-20 | 2018-03-06 | 中国农业大学 | Unmanned aerial vehicle onboard is precisely to target seeding system and operational method |
KR20190075473A (en) * | 2017-12-21 | 2019-07-01 | 한국해양과학기술원 | Apparatus for direct seeding using drone |
CN208593497U (en) * | 2018-07-31 | 2019-03-12 | 宁夏翼航智控科技有限公司 | A kind of plant protection drone |
CN208993929U (en) * | 2018-09-30 | 2019-06-18 | 广州极飞科技有限公司 | A kind of material spreading gear and unmanned plane |
CN109665103A (en) * | 2019-01-14 | 2019-04-23 | 珠海卡特瑞科农林航空装备研究所有限公司 | Seeding apparatus and sowing unmanned plane with the device |
Non-Patent Citations (1)
Title |
---|
钱如竹: "《农业实用电子仪器精选》", 人民邮电出版社 * |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112238943A (en) * | 2020-10-20 | 2021-01-19 | 鲁莺 | Agricultural seeding unmanned aerial vehicle of deviation is prevented in ration input |
CN112238943B (en) * | 2020-10-20 | 2022-05-27 | 北京麦麦趣耕科技有限公司 | Agricultural seeding unmanned aerial vehicle of deviation is prevented in ration input |
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