CN108082465B - Remote control unmanned aerial vehicle seeding device and seeding method thereof - Google Patents
Remote control unmanned aerial vehicle seeding device and seeding method thereof Download PDFInfo
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- CN108082465B CN108082465B CN201810012193.0A CN201810012193A CN108082465B CN 108082465 B CN108082465 B CN 108082465B CN 201810012193 A CN201810012193 A CN 201810012193A CN 108082465 B CN108082465 B CN 108082465B
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/20—Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
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- A—HUMAN NECESSITIES
- A01—AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
- A01C—PLANTING; SOWING; FERTILISING
- A01C7/00—Sowing
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/13—Propulsion using external fans or propellers
- B64U50/14—Propulsion using external fans or propellers ducted or shrouded
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- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
Abstract
The invention discloses a remote control unmanned aerial vehicle seeding device and a seeding method thereof, wherein the seeding device mainly comprises: unmanned aerial vehicle and remote controller, unmanned aerial vehicle mainly includes: the system comprises a Bluetooth module, a PCL controller, an inverter, a protection device, an engine, an air extractor, a pressure pump, a seed cabin and an air compression cannon, wherein the Bluetooth module is installed on the upper layer of the unmanned aerial vehicle close to the head of the unmanned aerial vehicle; the invention has novel structure, lower cost and comprehensive functions, effectively solves the problems which can not be solved by partial prior art, improves the efficiency compared with the products of the same type and is suitable for wide popularization.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicle seeding, in particular to a remote control unmanned aerial vehicle seeding device and a seeding method thereof.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer.
Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.
With the increasing input subsidy of the country to agriculture, modern plant protection machines are entering the hands of farmers. The plant protection machine overcomes the defects of labor force, and improves the production efficiency and the agricultural precision. Plant protection is an important component of agriculture and forestry production. Is one of the important measures for ensuring high yield and high harvest of agriculture and forestry. In order to economically and effectively protect plants, various control methods and positive effects are exerted, the policy of 'prevention mainly and comprehensive control' is implemented, and diseases, insects, weeds and other harmful organisms are eliminated before the harmful organisms are damaged, so that the harmful organisms are prevented from being damaged.
Plant protection unmanned aerial vehicle, as the name implies is the unmanned aircraft who is used for agriculture and forestry plant protection operation.
However, in the prior art, the seeds sowed by the unmanned aerial vehicle are often eaten by flying birds, so that the sowing effect is greatly influenced, and part of the seeds cannot be buried in the soil.
Disclosure of Invention
Aiming at the technical problems, the invention provides a remote control unmanned aerial vehicle seeding device and a seeding method thereof, which can effectively inject seeds into soil to be seeded and dispel nearby flying birds, so that the flying birds are prevented from predating the seeds.
The technical scheme of the invention is as follows: the utility model provides a remote control unmanned aerial vehicle seeder mainly includes: unmanned aerial vehicle and remote controller, unmanned aerial vehicle includes: main duct, tail duct, unmanned aerial vehicle antenna, camera device, support, bluetooth module, sensing receiver, GPRS module, stand-by power supply, PCL controller, dc-to-ac converter, two-dimensional linkage controller, storage battery, protection device, engine, air exhaust device, force pump, kind storehouse, left duct, right duct, solar cell panel, air compression big gun, main duct is located the unmanned aerial vehicle middle part, and main duct includes: the unmanned aerial vehicle comprises main culvert propellers, main culvert motors and main culvert supports, wherein the number of the main culvert propellers is four, the main culvert propellers are uniformly arranged on the main culvert motors along the circumferential direction, the main culvert motors are arranged on the main culvert supports, and the main culvert supports are connected with the unmanned aerial vehicle; the tail duct is located the unmanned aerial vehicle afterbody, and the tail duct includes: the tail culvert motor is arranged behind the tail culvert support, the tail culvert rotating shaft is arranged behind the tail culvert motor, and the number of the tail culvert propellers is three and is uniformly arranged on the tail culvert rotating shaft along the circumferential direction; unmanned aerial vehicle antenna mounting is close to aircraft nose department in the unmanned aerial vehicle top, camera device installs and is close to aircraft nose department in the unmanned aerial vehicle bottom, and camera device includes: the camera is mounted at the front end of the camera, the camera is mounted at the front end of the left motor and the right motor, the left motor and the right motor are connected with the bottom end of the connecting rod, the top end of the connecting rod is connected with the front ends of the upper motor and the lower motor, and the upper motor and the lower motor are mounted at the bottom of the unmanned aerial vehicle and close to the nose; the support totally four, evenly install in unmanned aerial vehicle bottom, bluetooth module installs in the unmanned aerial vehicle upper strata and is close to the aircraft nose department, the sensing receiver is installed in the bluetooth module rear, the GPRS module is installed on the sensing receiver, stand-by power supply installs in the sensing receiver rear, the PCL controller is installed in stand-by power supply rear, dc-to-ac converter installation and PCL controller rear, storage battery installs in the dc-to-ac converter rear, two-dimensional linkage control installs in the storage battery top, protection device installs in unmanned aerial vehicle top and is close to aircraft tail department, and protection device includes: the parachute system is installed below the second electromagnetic valve, and the second electromagnetic valve is installed at the position, close to the tail, of the top in the unmanned aerial vehicle; the engine is located unmanned aerial vehicle lower floor middle part, air exhaust device is located unmanned aerial vehicle lower floor internal surface and is close to tail department, and air exhaust device includes: the air exhaust pipe is connected with the filter screen at one end, the other end of the air exhaust pipe is connected with the pressure pump, and the filter screen is positioned on the inner surface of the lower layer of the unmanned aerial vehicle and close to the tail of the unmanned aerial vehicle; be equipped with air inlet and gas outlet on the force pump, the air inlet is installed in force pump rear bottom, the gas outlet is installed in force pump front end middle part, the kind storehouse is located the interior lower floor of unmanned aerial vehicle and is close to the aircraft nose department, and the kind storehouse includes: the seed box is positioned in the seed bin, the seed inlet is mounted at the top of the front end of the seed box and connected with the unmanned aerial vehicle, the conveying crawler is mounted at the bottom of the seed bin, and the second electromagnetic valve is mounted behind the conveying crawler; left duct is installed on the unmanned aerial vehicle left wing, and left duct includes: the unmanned aerial vehicle comprises three left culvert propellers, a left culvert motor, a left culvert rotating shaft and a left culvert support, wherein the left culvert propellers are uniformly arranged on the left culvert rotating shaft, the left culvert rotating shaft is arranged above the left culvert motor, the left culvert motor is arranged on the left culvert support, and the left culvert support is connected with the unmanned aerial vehicle; right duct is installed on the unmanned aerial vehicle right wing, and right duct includes: the unmanned aerial vehicle comprises right culvert propellers, a right culvert motor, a right culvert rotating shaft and a right culvert support, wherein the number of the right culvert propellers is three, the right culvert propellers are uniformly arranged on the right culvert rotating shaft, the right culvert rotating shaft is arranged above the right culvert motor, the right culvert motor is arranged on the right culvert support, and the right culvert support is connected with the unmanned aerial vehicle; solar cell panel totally two, install respectively on the wing about unmanned aerial vehicle, the air compression big gun is installed between force pump and kind storehouse and is connected with kind storehouse with the force pump respectively, and the air compression big gun includes: the air cabin is arranged below the air outlet, the third electromagnetic valve is arranged below the air cabin, the front end of the air outlet is connected with the seed box, the rear part of the air outlet is connected with the transmitting pipe, and the transmitting pipe is arranged below the third electromagnetic valve; the PCL controller is respectively connected with the main duct, the tail duct, the camera device, the Bluetooth module, the sensing receiver, a standby power supply, the inverter, the engine, the air extractor, the pressure pump, the seed bin, the left duct, the right duct and the air compression cannon through data lines, the solar cell panel is connected with the two-dimensional linkage controller through a wire, the two-dimensional linkage controller is connected with the storage battery pack through a wire, the storage battery pack is connected with the inverter through a wire, the engine is respectively connected with the main duct, the tail duct, the camera device, the air extractor, the pressure pump, the seed bin, the left duct, the right duct and the air compression cannon through wires, and the sensing receiver is respectively connected with an unmanned aerial vehicle antenna and the camera and the GPRS module; the unmanned aerial vehicle antenna is connected with the remote controller through wireless.
Further, the forward flying speed of the unmanned aerial vehicle during working is 50-60 m/min; the phenomenon that planting space is wasted due to the fact that the seeding interval is large after the speed is too high and the growth of crops with the seeding interval being small due to too slow speed is mutually influenced is prevented.
Furthermore, the working frequency of the air compression cannon is 60 times/min, and the seeds are shot into the land through the air compression cannon, so that the growth distance between crops is just met by 60 times/min while the successful growth probability of the seeds is ensured.
Further, the protection device automatically works when the descending speed exceeds 20 m/s; prevent that this device from dropping when the high altitude meets accident, not only guaranteed below passerby safety, more effectively prevent unmanned aerial vehicle's damage.
Further, the working method of the device is as follows:
a. a preparation stage: an operator fills seeds in the seed box through the seed inlet arranged in the seed cabin, and then checks whether the signal connection between the unmanned aerial vehicle and the remote controller is successful;
b. flying to the working site: an operator firstly inputs a working place in the remote controller, then presses down the key position for reaching the working place on the remote controller, the unmanned aerial vehicle controls the main duct, the tail duct, the engine, the left duct and the right duct to work and automatically fly to a specified position according to the GPRS module and the PCL controller, and then the progress of the unmanned aerial vehicle flying to the working place is observed by observing the positioning display screen;
c. and (3) starting to work: the operator adjusts the observation angle of the camera through the lens raising key position, the lens descending key position, the lens left turning key position and the lens right turning key position, observes the working environment of the unmanned aerial vehicle through the image display screen, controls the movement of the unmanned aerial vehicle through the advancing key position, the retreating key position, the left flying key position and the right flying key position, and controls the seeding work of the unmanned aerial vehicle through the air compression gun working key position and the air compression gun stopping key position;
d. returning: after the work is finished, the operator passes through on the remote controller return the key position and issue the instruction of returning a voyage, then through observing the positioning display screen observes unmanned aerial vehicle and returns a voyage progress.
Compared with the prior art, the invention has the beneficial effects that:
1. the invention effectively solves the technical problem that the seeds can not be planted in the land in the prior art, and the seeds are injected into the land by the air compression cannon to a certain depth, thereby ensuring the successful growth probability of the seeds.
2. The invention is provided with the protection device to prevent the invention from falling off when accidents happen at high altitude, thereby not only ensuring the safety of people below the vehicle, but also effectively preventing the user from generating great loss.
3. The invention effectively solves the problem that the flying birds infringe the land which is just sowed in the prior art, and the flying birds around the land are dispelled by the sound generated by the air compression cannon, thereby increasing the land yield.
4. The invention has novel structure, lower cost and comprehensive functions, effectively solves the problems which can not be solved by partial prior art, improves the efficiency compared with the products of the same type and is suitable for wide popularization.
Drawings
Fig. 1 is an external view of the drone of the present invention;
fig. 2 is a schematic structural diagram of the drone of the present invention;
FIG. 3 is a schematic diagram of the controller of the present invention;
1-unmanned aerial vehicle, 2-remote controller, 3-main duct, 4-tail duct, 5-unmanned aerial vehicle antenna, 6-camera device, 7-bracket, 8-Bluetooth module, 9-sensing receiver, 10-GPRS module, 11-standby power supply, 12-PCL controller, 13-inverter, 14-two-dimensional linkage controller, 15-storage battery, 16-protective device, 17-engine, 18-air extractor, 19-pressure pump, 20-seed bin, 21-left duct, 22-right duct, 23-solar panel, 24-air compression gun, 201-switch key position, 202-working location key position, 203-image display screen, 204-lens raising key position, 205-lens lowering key position, 206-lens left turn key position, 207-lens right turn key position, 208-standby power supply turn-on key position, 209-air compression cannon work key position, 210-air compression cannon stop key position, 211-protective device turn-on key position, 212-advance key position, 213-retreat key position, 214-left fly key position, 215-right fly key position, 216-positioning display screen, 217-return navigation key position, 218-remote controller antenna, 301-main culvert propeller, 302-main culvert motor, 303-main culvert support, 401-tail culvert support, 402-tail culvert motor, 403-tail culvert rotating shaft, 404-tail culvert propeller, 601-lens, 602-camera, 603-left and right motors, 604-connecting rod, 605-up and down motors, 1601-parachute system, 1602-electromagnetic valve-umbrella, 1801-air exhaust pipe, 1802-filter screen, 1901-air inlet, 1902-air outlet, 2001-seed box, 2002-seed inlet, 2003-conveying crawler belt, 2004-electromagnetic valve II, 2101-left culvert propeller, 2102-left culvert motor, 2103-left culvert rotating shaft, 2104-left culvert bracket, 2201-right culvert propeller, 2202-right culvert motor, 2203-right culvert rotating shaft, 2204-right culvert bracket, 2401-air cabin, 2402-electromagnetic valve III, 2403-seed outlet, 2404-launching tube.
Detailed Description
In order to explain the implementation of the invention more fully, the following implementation examples of the remote control unmanned aerial vehicle seeding device and the seeding method thereof are provided. These examples are merely illustrative and do not limit the scope of the invention. The invention is further illustrated by the following exemplary embodiments.
Example 1:
as shown in fig. 1, a remote control unmanned aerial vehicle seeder mainly includes: unmanned aerial vehicle 1 and remote controller 2, unmanned aerial vehicle 1 includes: main duct 3, tail duct 4, unmanned aerial vehicle antenna 5, camera device 6, support 7, bluetooth module 8, sensing receiver 9, GPRS module 10, stand-by power supply 11, PCL controller 12, dc-to-ac converter 13, two-dimensional coordinated control 14, storage battery 15, protection device 16, engine 17, air exhaust device 18, force pump 19, kind storehouse 20, left duct 21, right duct 22, solar cell panel 23, air compression big gun 24, main duct 3 is located 3 middle parts of unmanned aerial vehicle, main duct 3 includes: the unmanned aerial vehicle comprises main culvert propellers 301, main culvert motors 302 and main culvert supports 303, wherein the number of the main culvert propellers 301 is four, the main culvert propellers are uniformly arranged on the main culvert motors 302 along the circumferential direction, the main culvert motors 302 are arranged on the main culvert supports 303, and the main culvert supports 303 are connected with the unmanned aerial vehicle 1; tail duct 4 is located 1 afterbody of unmanned aerial vehicle, and tail duct 4 includes: the unmanned aerial vehicle comprises a tail culvert support 401, a tail culvert motor 402, a tail culvert rotating shaft 403 and tail culvert propellers 404, wherein the tail culvert support 401 is installed at the tail of the unmanned aerial vehicle 1, the tail culvert motor 402 is installed behind the tail culvert support 401, the tail culvert rotating shaft 403 is installed behind the tail culvert motor 402, and the tail culvert propellers 404 are three in number and are uniformly installed on the tail culvert rotating shaft 403 along the circumferential direction; unmanned aerial vehicle antenna 5 is installed and is close to aircraft nose department at 1 top of unmanned aerial vehicle, and camera device 6 is installed and is close to aircraft nose department in 1 bottom of unmanned aerial vehicle, and camera device 6 includes: the camera comprises a lens 601, a camera 602, a left motor 603, a right motor 603, a connecting rod 604 and an up-down motor 605, wherein the lens 601 is installed at the front end of the camera 602, the camera 602 is installed at the front end of the left motor 603 and the right motor 603, the left motor 603 and the right motor 603 are connected with the bottom end of the connecting rod 604, the top end of the connecting rod 604 is connected with the front end of the up-down motor 605, and the up-down motor; support 7 is totally four, evenly install in 1 bottom of unmanned aerial vehicle, bluetooth module 8 is installed and is close to aircraft nose department in 1 upper strata of unmanned aerial vehicle, sensing receiver 9 is installed in 8 rear of bluetooth module, GPRS module 10 is installed on sensing receiver 9, stand-by power supply 11 is installed in 9 rear of sensing receiver, PCL controller 12 is installed in 11 rear of stand-by power supply, 13 installation of dc-to-ac converter and 12 rear of PCL controller, storage battery 15 is installed in 13 rear of dc-to-ac converter, two-dimensional linkage control 14 is installed in storage battery 15 top, protection device 16 installs top in unmanned aerial vehicle 1 and is close to aircraft tail department, protection device 16 includes: the parachute system 1601 is installed below the electromagnetic valve II 1602, and the electromagnetic valve II 1602 is installed at the top of the unmanned aerial vehicle 1 near the tail; engine 17 is located 1 interior lower floor middle part of unmanned aerial vehicle, and air exhaust device 18 is located 1 lower floor internal surface of unmanned aerial vehicle and is close to tail department, and air exhaust device 18 includes: the exhaust pipe 1801 is connected with the filter screen 1802, one end of the exhaust pipe 1801 is connected with the filter screen 1802, the other end of the exhaust pipe 1801 is connected with the pressure pump 19, and the filter screen 1802 is located on the inner surface of the lower layer of the unmanned aerial vehicle 1 and close to the tail of the unmanned aerial vehicle; be equipped with air inlet 1901 and gas outlet 1902 on the force pump 19, air inlet 1901 is installed in force pump 19 rear bottom, and gas outlet 1902 is installed in force pump 19 front end middle part, and the lower floor is close to the aircraft nose department in the kind storehouse 20 is located unmanned aerial vehicle 1, and kind storehouse 20 includes: the unmanned aerial vehicle comprises a seed box 2001, a seed inlet 2002, a conveying crawler 2003 and a second electromagnetic valve 2004, wherein the seed box 2001 is positioned in a seed cabin 20, the seed inlet 2002 is installed at the top of the front end of the seed box 2001 and is connected with the unmanned aerial vehicle 1, the conveying crawler 2003 is installed at the bottom of the seed cabin 2001, and the second electromagnetic valve 2004 is installed behind the conveying crawler 2003; left duct 21 installs on unmanned aerial vehicle 1 left wing, and left duct 21 includes: the unmanned aerial vehicle comprises three left culvert propellers 2101, three left culvert motors 2102, three left culvert rotating shafts 2103 and a left culvert support 2104, wherein the left culvert propellers 2101 are uniformly arranged on the left culvert rotating shafts 2103, the left culvert rotating shafts 2103 are arranged above the left culvert motors 2102, the left culvert motors 2102 are arranged on the left culvert support 2104, and the left culvert support 2104 is connected with the unmanned aerial vehicle 1; right duct 21 installs on unmanned aerial vehicle 1 right wing, and right duct 22 includes: the unmanned aerial vehicle comprises three right culvert propellers 2201, a right culvert motor 2202, a right culvert rotating shaft 2203 and a right culvert support 2204, wherein the number of the right culvert propellers 2201 is three, the right culvert rotating shaft 2203 is uniformly arranged on the right culvert rotating shaft 2203, the right culvert rotating shaft 2203 is arranged above the right culvert motor 2202, the right culvert motor 2202 is arranged on the right culvert support 2204, and the right culvert support 2204 is connected with the unmanned aerial vehicle 1; solar cell panel 23 is two totally, installs respectively on unmanned aerial vehicle 1 left and right sides wing, and air compression big gun 24 is installed between force pump 19 and kind storehouse 20 and is connected with force pump 19 and kind storehouse 20 respectively, and air compression big gun 24 includes: the air cabin 2401 is arranged below the air outlet 1902, the three electromagnetic valves 2402 are arranged below the air cabin 2401, the front ends of the air outlet 2403 are connected with the seed box 2001, the rear ends of the air outlet 2403 are connected with the emission tube 2404, and the emission tube 2404 is arranged below the three electromagnetic valves 2402; the PCL controller 12 is respectively connected with the main duct 3, the tail duct 4, the camera device 6, the Bluetooth module 8, the sensing receiver 9, the standby power supply 11, the inverter 13, the engine 17, the air extractor 18, the pressure pump 19, the seed cabin 20, the left duct 21, the right duct 22 and the air compression cannon 24 through data lines, the solar cell panel 23 is connected with the two-dimensional linkage controller 14 through a wire, the two-dimensional linkage controller 14 is connected with the storage battery pack 15 through a wire, the storage battery pack 15 is connected with the inverter 13 through a wire, the engine 17 is respectively connected with the main duct 3, the tail duct 4, the camera device 6, the air extractor 18, the pressure pump 19, the seed cabin 20, the left duct 21, the right duct 22 and the air compression cannon 24 through wires, and the sensing receiver 9 is respectively connected with the unmanned aerial vehicle antenna 5 and the camera 6 and the GPRS module 10; the unmanned aerial vehicle antenna 5 is connected with the remote controller 2 through wireless.
Wherein the forward flying speed of the unmanned aerial vehicle 1 during working is 60 m/min; the situation that planting space is wasted due to the fact that the seeding interval is large after the speed is too high and crop growth is influenced due to the fact that the seeding interval is small after the speed is too low is prevented; the working frequency of the air compression cannon 24 is 60 times/min, and the seeds are injected into the land through the air compression cannon 24, so that the growth distance between crops is just met by 60 times/min while the successful growth probability of the seeds is ensured; the protection device 16 automatically works when the descending speed exceeds 20 m/s; the device is prevented from falling off when accidents happen at high altitude, so that the safety of passers-by below is guaranteed, and the user is more effectively prevented from generating great loss.
The working method of the device comprises the following steps:
a. a preparation stage: an operator fills the seed box 2001 with seeds through a seed inlet 2002 arranged in the seed cabin 20, and then checks whether the signal connection between the unmanned aerial vehicle 1 and the remote controller 2 is successful;
b. flying to the working site: an operator firstly inputs a working place in the remote controller 2, then presses a key position 202 for reaching the working place on the remote controller 2, the unmanned aerial vehicle 1 controls the main duct 3, the tail duct 4, the engine 17, the left duct 21 and the right duct 22 to work according to the GPRS module 10 and the PCL controller 12 to automatically fly to a specified position, and then the progress of the unmanned aerial vehicle 1 flying to the working place is observed through the observation and positioning display screen 216;
c. and (3) starting to work: the operator adjusts the observation angle of the camera 6 through the lens raising key 204, the lens lowering key 205, the lens left turning key 206 and the lens right turning key 207, and observes the working environment of the unmanned aerial vehicle 1 through the image display screen 203, then controls the movement of the unmanned aerial vehicle 1 through the forward key 212, the backward key 213, the left flying key 214 and the right flying key 215, and finally controls the seeding work of the unmanned aerial vehicle 1 through the air compression cannon working key 209 and the air compression cannon stop key 210;
d. returning: after the work is finished, the operator gives a return instruction through the return key position 217 on the remote controller 2, and then observes the return progress of the unmanned aerial vehicle 1 through observing the positioning display screen 216.
Finally, it should be noted that: the above examples are only intended to illustrate the technical solution of the present invention, but not to limit it; although the present invention has been described in detail with reference to the foregoing embodiments, it will be understood by those of ordinary skill in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some technical features may be equivalently replaced; and such modifications or substitutions do not depart from the spirit and scope of the corresponding technical solutions of the embodiments of the present invention.
Claims (6)
1. The utility model provides a remote control unmanned aerial vehicle seeder which characterized in that includes: unmanned aerial vehicle (1), remote controller (2), main duct (3), tail duct (4), unmanned aerial vehicle antenna (5), camera device (6), support (7), bluetooth module (8), sensing receiver (9), GPRS module (10), stand-by power supply (11), PCL controller (12), dc-to-ac converter (13), two-dimentional coordinated control ware (14), storage battery (15), protection device (16), engine (17), air exhaust device (18), force pump (19), kind storehouse (20), left duct (21), right duct (22), solar cell panel (23), air compression big gun (24), main duct (3) are located unmanned aerial vehicle (3) middle part, main duct (3) include: the unmanned aerial vehicle comprises main culvert propellers (301), main culvert motors (302) and main culvert supports (303), wherein the number of the main culvert propellers (301) is four, the main culvert propellers are uniformly arranged on the main culvert motors (302) along the circumferential direction, the main culvert motors (302) are arranged on the main culvert supports (303), and the main culvert supports (303) are connected with the unmanned aerial vehicle (1); tail duct (4) are located unmanned aerial vehicle (1) afterbody, and tail duct (4) include: the unmanned aerial vehicle tail culvert device comprises a tail culvert support (401), tail culvert motors (402), tail culvert rotating shafts (403) and tail culvert propellers (404), wherein the tail culvert support (401) is installed at the tail of the unmanned aerial vehicle (1), the tail culvert motors (402) are installed behind the tail culvert support (401), the tail culvert rotating shafts (403) are installed behind the tail culvert motors (402), and the number of the tail culvert propellers (404) is three and the tail culvert propellers are uniformly installed on the tail culvert rotating shafts (403) along the circumferential direction; unmanned aerial vehicle antenna (5) are installed and are close to aircraft nose department at unmanned aerial vehicle (1) top, camera device (6) are installed and are close to aircraft nose department in unmanned aerial vehicle (1) bottom, and camera device (6) include: the camera comprises a lens (601), a camera (602), a left motor (603), a right motor (603), a connecting rod (604) and an upper motor (605), wherein the lens (601) is installed at the front end of the camera (602), the camera (602) is installed at the front end of the left motor (603) and the right motor (603), the left motor (603) and the right motor (603) are connected with the bottom end of the connecting rod (604), the top end of the connecting rod (604) is connected with the front end of the upper motor (605), and the upper motor (605) and the lower motor (605) are installed at; support (7) totally four, evenly install in unmanned aerial vehicle (1) bottom, bluetooth module (8) are installed and are close to the aircraft nose department in unmanned aerial vehicle (1) upper strata, install in bluetooth module (8) rear in sensing receiver (9), install on sensing receiver (9) GPRS module (10), stand-by power supply (11) are installed in sensing receiver (9) rear, install in stand-by power supply (11) rear PCL controller (12), inverter (13) installation and PCL controller (12) rear, install in inverter (13) rear storage battery (15), two-dimensional linkage controller (14) are installed in storage battery (15) top, protection device (16) are installed and are close to aircraft tail department in unmanned aerial vehicle (1) top, and protection device (16) include: the parachute system (1601) and the second electromagnetic valve (1602), the parachute system (1601) is installed below the second electromagnetic valve (1602), and the second electromagnetic valve (1602) is installed at the position, close to the tail, of the top in the unmanned aerial vehicle (1); engine (17) are located unmanned aerial vehicle (1) lower floor middle part, air exhaust device (18) are located unmanned aerial vehicle (1) lower floor internal surface and are close to tail department, and air exhaust device (18) include: the air exhaust pipe (1801) is connected with the filter screen (1802), one end of the air exhaust pipe (1801) is connected with the filter screen (1802), the other end of the air exhaust pipe is connected with the pressure pump (19), and the filter screen (1802) is located on the inner surface of the lower layer of the unmanned aerial vehicle (1) and close to the tail of the unmanned aerial vehicle; be equipped with air inlet (1901) and gas outlet (1902) on force pump (19), install in force pump (19) rear bottom air inlet (1901), install in force pump (19) front end middle part gas outlet (1902), plant storehouse (20) and be located unmanned aerial vehicle (1) lower floor and be close to the aircraft nose department, plant storehouse (20) and include: the seed box (2001) is positioned in the seed bin (20), the seed inlet (2002) is mounted at the top of the front end of the seed box (2001) and connected with the unmanned aerial vehicle (1), the conveying crawler (2003) is mounted at the bottom of the seed bin (2001), and the second electromagnetic valve (2004) is mounted behind the conveying crawler (2003); left duct (21) are installed on unmanned aerial vehicle (1) left wing, and left duct (21) include: the unmanned aerial vehicle comprises three left culvert propellers (2101), three left culvert motors (2102), a left culvert rotating shaft (2103) and a left culvert support (2104), wherein the three left culvert propellers (2101) are uniformly arranged on the left culvert rotating shaft (2103), the left culvert rotating shaft (2103) is arranged above the left culvert motor (2102), the left culvert motor (2102) is arranged on the left culvert support (2104), and the left culvert support (2104) is connected with the unmanned aerial vehicle (1); right duct (22) are installed on unmanned aerial vehicle (1) right wing, and right duct (22) include: the unmanned aerial vehicle comprises right culvert propellers (2201), right culvert motors (2202), right culvert rotating shafts (2203) and right culvert supports (2204), wherein the number of the right culvert propellers (2201) is three, the right culvert propellers are uniformly arranged on the right culvert rotating shafts (2203), the right culvert rotating shafts (2203) are arranged above the right culvert motors (2202), the right culvert motors (2202) are arranged on the right culvert supports (2204), and the right culvert supports (2204) are connected with the unmanned aerial vehicle (1); solar cell panel (23) totally two, install respectively on unmanned aerial vehicle (1) left and right sides wing, air compression big gun (24) are installed between force pump (19) and kind storehouse (20) and are connected with kind storehouse (20) with force pump (19) respectively, and air compression big gun (24) include: the air tank (2401), the three electromagnetic valves (2402), the seed outlet (2403) and the emission tube (2404), wherein the air tank (2401) is installed below the seed outlet (1902), the three electromagnetic valves (2402) are installed below the air tank (2401), the front end of the seed outlet (2403) is connected with the seed box (2001), the rear end of the seed outlet is connected with the emission tube (2404), and the emission tube (2404) is installed below the three electromagnetic valves (2402); the PCL controller (12) is respectively connected with the main duct (3), the tail duct (4), the camera device (6), the Bluetooth module (8), the sensing receiver (9), the standby power supply (11), the inverter (13), the engine (17), the air extracting device (18), the pressure pump (19), the seed bin (20), the left duct (21), the right duct (22) and the air compression cannon (24) through data lines, the solar cell panel (23) is connected with the two-dimensional linkage controller (14) through a wire, the two-dimensional linkage controller (14) is connected with the storage battery pack (15) through a wire, the storage battery pack (15) is connected with the inverter (13) through a wire, the engine (17) is respectively connected with the main duct (3), the tail duct (4), the camera device (6), the air extracting device (18), the pressure pump (19), the seed bin (20), the left duct (21) and the engine, The right duct (22) is connected with the air compression cannon (24), and the sensing receiver (9) is respectively connected with the unmanned aerial vehicle antenna (5), the camera (6) and the GPRS module (10); the unmanned aerial vehicle antenna (5) is connected with the remote controller (2) in a wireless mode.
2. The seeding device of claim 1, wherein the remote controller (2) has a switch key (201), a go-to-work location key (202), an image display screen (203), a lens raising key (204), a lens lowering key (205), a lens left-turning key (206), a lens right-turning key (207), a battery backup starting key (208), an air compression gun working key (209), an air compression gun stopping key (210), a protector starting key (211), a forward key (212), a backward key (213), a left-flying key (214), a right-flying key (215), a positioning display screen (216), and a backward key (217), the top of the remote controller (2) is provided with a remote controller antenna (218), the remote controller (2) is further provided with a wireless transmitter and a wireless receiver, the wireless transmitter and the wireless receiver are connected to the unmanned aerial vehicle antenna (218) and the unmanned aerial vehicle antenna (218) 1) The sensing receiver (9) in the sensor is connected with a GPRS module (10).
3. A remote-controlled drone sowing device according to claim 1, characterised in that the forward flying speed of the drone (1) in operation is 50-60 m/min.
4. A remote-controlled unmanned aerial vehicle seeding device according to claim 1, wherein the operating frequency of the air compression cannon (24) is 60 times/min.
5. A remote-controlled drone sowing device according to claim 1, characterised in that the protection device (16) operates automatically when the descent speed exceeds 20 m/s.
6. A remote-controlled drone seeding device according to claim 2, characterised in that the working method of the device is:
a. a preparation stage: an operator fills the seed box (2001) with seeds through the seed inlet (2002) arranged in the seed cabin (20), and then checks whether the signal connection between the unmanned aerial vehicle (1) and the remote controller (2) is successful;
b. flying to the working site: an operator firstly inputs a working place in the remote controller (2), then presses down the key position (202) of the working place on the remote controller (2), the unmanned aerial vehicle (1) controls the main duct (3), the tail duct (4), the engine (17), the left duct (21) and the right duct (22) to work and automatically fly to a specified position according to the GPRS module (10) and the PCL controller (12), and then the progress of the unmanned aerial vehicle (1) flying to the working place is observed by observing the positioning display screen (216);
c. and (3) starting to work: an operator adjusts the observation angle of the camera (6) through the lens raising key (204), the lens descending key (205), the lens left turning key (206) and the lens right turning key (207), observes the working environment of the unmanned aerial vehicle (1) through the image display screen (203), controls the movement of the unmanned aerial vehicle (1) through the advancing key (212), the retreating key (213), the left flying key (214) and the right flying key (215), and controls the seeding work of the unmanned aerial vehicle (1) through the air compression gun working key (209) and the air compression gun stopping key (210);
d. returning: after work is finished, an operator gives a return flight instruction through the return flight key position (217) on the remote controller (2), and then observes the return flight progress of the unmanned aerial vehicle (1) through observing the positioning display screen (216).
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| CN201810012193.0A CN108082465B (en) | 2018-01-05 | 2018-01-05 | Remote control unmanned aerial vehicle seeding device and seeding method thereof |
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| CN108966757A (en) * | 2018-06-21 | 2018-12-11 | 怀宁县涛涛家庭农场 | A kind of full-automatic agricultural seeding machine |
| CN109151404A (en) * | 2018-10-30 | 2019-01-04 | 国网四川省电力公司广元供电公司 | A electric network operation scene inspection system anti-violating the regulations |
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| KR101354646B1 (en) * | 2011-11-17 | 2014-01-22 | 재단법인대구경북과학기술원 | Flying Robots with Flight Angle Control function based on Solar Cells |
| US9382003B2 (en) * | 2013-03-24 | 2016-07-05 | Bee Robotics Corporation | Aerial farm robot system for crop dusting, planting, fertilizing and other field jobs |
| US20150274289A1 (en) * | 2014-03-31 | 2015-10-01 | The Boeing Corporation | Vertically landing aircraft |
| CN104255137B (en) * | 2014-09-09 | 2016-03-30 | 湖南星索尔航空科技有限公司 | A kind of precision drilling operating system based on unmanned aerial vehicle platform and method |
| CN105173084B (en) * | 2015-10-29 | 2016-12-28 | 黑龙江科技大学 | A kind of unmanned plane plant seeds by airplane device |
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