CN107310724B - Intelligent unmanned aerial vehicle used for wind power generation and capable of sowing - Google Patents
Intelligent unmanned aerial vehicle used for wind power generation and capable of sowing Download PDFInfo
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- CN107310724B CN107310724B CN201710476592.8A CN201710476592A CN107310724B CN 107310724 B CN107310724 B CN 107310724B CN 201710476592 A CN201710476592 A CN 201710476592A CN 107310724 B CN107310724 B CN 107310724B
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- Prior art keywords
- power generation
- unmanned aerial
- aerial vehicle
- machine body
- assembly
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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
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
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- A—HUMAN NECESSITIES
- A01—AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
- A01C—PLANTING; SOWING; FERTILISING
- A01C7/00—Sowing
- A01C7/08—Broadcast seeders; Seeders depositing seeds in rows
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D5/00—Other wind motors
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D9/00—Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations
- F03D9/20—Wind motors characterised by the driven apparatus
- F03D9/25—Wind motors characterised by the driven apparatus the apparatus being an electrical generator
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D9/00—Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations
- F03D9/30—Wind motors specially adapted for installation in particular locations
- F03D9/32—Wind motors specially adapted for installation in particular locations on moving objects, e.g. vehicles
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/14—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries for charging batteries from dynamo-electric generators driven at varying speed, e.g. on vehicle
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/32—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries for charging batteries from a charging set comprising a non-electric prime mover rotating at constant speed
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K35/00—Generators with reciprocating, oscillating or vibrating coil system, magnet, armature or other part of the magnetic circuit
- H02K35/04—Generators with reciprocating, oscillating or vibrating coil system, magnet, armature or other part of the magnetic circuit with moving coil systems and stationary magnets
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K7/00—Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
- H02K7/18—Structural association of electric generators with mechanical driving motors, e.g. with turbines
- H02K7/1807—Rotary generators
- H02K7/1823—Rotary generators structurally associated with turbines or similar engines
- H02K7/183—Rotary generators structurally associated with turbines or similar engines wherein the turbine is a wind turbine
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- 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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- 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
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
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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
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/72—Wind turbines with rotation axis in wind direction
-
- 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
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/728—Onshore wind turbines
-
- 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 invention relates to an intelligent unmanned aerial vehicle capable of generating power by wind power and sowing, which comprises a machine body, a central control mechanism, a micro power generation mechanism and a flight mechanism, wherein the micro power generation mechanism comprises a fan blade, a rotating shaft, a spring and a first power generation assembly, a second power generation assembly is arranged below the machine body, the first power generation assembly and the second power generation assembly respectively comprise a power generation unit, the power generation unit comprises a moving coil, two electromagnets, a rectifier and a storage battery, the sowing mechanism comprises a storage box, a driving assembly, a stirring assembly and a discharge pipe, the driving assembly comprises a second driving shaft, a first gear and a second paddle, the stirring assembly comprises a worm and a stirring paddle, and a switch mechanism is arranged inside the storage box. This an intelligent unmanned aerial vehicle that is used for wind power generation and can sow, through miniature power generation mechanism, improved unmanned aerial vehicle's duration, through organism and second electricity generation subassembly's cooperation, realized the unmanned aerial vehicle electricity generation, through sowing mechanism, increased unmanned aerial vehicle's function, promoted unmanned aerial vehicle's practicality.
Description
Technical Field
The invention relates to the field of unmanned aerial vehicles, in particular to an intelligent unmanned aerial vehicle which is used for wind power generation and can be used for sowing.
Background
An unmanned aircraft, referred to as "drone", 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. Most unmanned aerial vehicle only is used for shooing the work usually, and the function is more single, has wasted very big resource, and unmanned aerial vehicle's continuation of the journey problem also is a problem moreover, these all greatly reduced unmanned aerial vehicle's practicality.
Disclosure of Invention
The technical problem to be solved by the invention is as follows: in order to overcome the not enough of prior art, provide an intelligent unmanned aerial vehicle that is used for wind power generation and can sow.
The technical scheme adopted by the invention for solving the technical problems is as follows: an intelligent unmanned aerial vehicle used for wind power generation and capable of sowing comprises a machine body, a middle control mechanism, a micro power generation mechanism and a flight mechanism, wherein the middle control mechanism is arranged on the machine body, the micro power generation mechanism is arranged on the periphery of the machine body, the flight mechanism is arranged on two sides of the machine body, and the micro power generation mechanism and the flight mechanism are both electrically connected with the middle control mechanism;
the micro power generation mechanism comprises fan blades, a rotating shaft, a spring and a first power generation assembly, wherein the fan blades are positioned outside the machine body and are uniformly arranged on the periphery of the rotating shaft;
a second power generation assembly is arranged below the machine body, and the first power generation assembly and the second power generation assembly both comprise power generation units;
the power generation unit comprises a moving coil, two electromagnets, a rectifier and a storage battery, wherein the moving coil is positioned between the two electromagnets, the polarities of the two electromagnets are opposite, the moving coil cuts magnetic induction lines of the electromagnets in the moving process, and the moving coil is electrically connected with the storage battery through the rectifier;
a connecting wire is arranged below the machine body, the machine body is connected with a moving coil of the second power generation assembly through the connecting wire, and the rotating shaft is connected with the moving coil of the first power generation assembly;
when needing the electricity generation, first motor starts, it is rotatory to drive first paddle, unmanned aerial vehicle takes the connecting wire to take off, because the wind-force resource of high latitude is very abundant, when unmanned aerial vehicle flies the take-off height, flight mechanism no longer works, at this moment, unmanned aerial vehicle relies on wind-force to float aloft through the connecting wire like the kite, unmanned aerial vehicle relies on the miniature power generation mechanism of organism whole body to carry out wind power generation, supply with self, the duration has been improved, and simultaneously, the connecting wire lower extreme is connected with the removal coil of second electricity generation subassembly, the connecting wire can drive the removal that removes the coil one on the other, at the in-process cutting magnetism induction line production electric current that reciprocates, input battery behind the rectifier. And, unmanned aerial vehicle detects the height from ground according to infrared distance meter, makes unmanned aerial vehicle remain throughout at a relatively stable height.
A seeding mechanism is further arranged below the machine body and comprises a storage box, a driving assembly, a stirring assembly and a discharge pipe, the driving assembly is arranged below the machine body and drives the stirring assembly to rotate in the storage box, the driving assembly comprises a second driving shaft, a first gear and a plurality of second blades, the second blades are uniformly arranged on the periphery of the second driving shaft, and the second driving shaft and the first gear are coaxially arranged;
the stirring assembly comprises a worm and a plurality of stirring paddles, the stirring paddles are positioned in the material storage box and are uniformly arranged on the periphery of the worm, and one end of the worm is positioned on one side of the first gear and is matched with the first gear;
the discharging pipe is arranged below the material storage box, and a switch mechanism is further arranged inside the material storage box.
When needs sow, start unmanned aerial vehicle, because wind-force, a plurality of second paddle can begin to rotate, and the second paddle drives the second drive shaft and rotates, also can rotate along with it with the coaxial first gear that sets up of second drive shaft, because first gear and worm one end match, so the worm begins to rotate, drives the stirring rake of the worm other end and rotates, has just so carried out the even stirring to the seed in the storage case. At the moment, the second motor is started to drive the first connecting rod to rotate, and because one end of the second connecting rod is hinged to the other end of the first connecting rod, the other end of the second connecting rod is in transmission connection with the sealing cover through the third connecting rod, the third connecting rod realizes horizontal movement through the limiting sleeve and drives the sealing cover to be opened and closed.
Preferably, the switch mechanism comprises a second motor, a third driving shaft, a first connecting rod, a second connecting rod, a third connecting rod and a sealing cover, the second motor is in transmission connection with the first connecting rod through the third driving shaft, one end of the first connecting rod is hinged to the third driving shaft, the other end of the first connecting rod is hinged to one end of the second connecting rod, the other end of the second connecting rod is in transmission connection with the sealing cover through the third connecting rod, and the sealing cover is arranged at the connection position of the material storage box and the material discharge pipe.
Preferably, in order to enable the sealing cover to move horizontally, a limiting sleeve is sleeved on the periphery of the third connecting rod and fixed inside the storage box.
Preferably, the flight mechanism comprises a first motor, a first driving shaft and a plurality of first blades, the first motor is fixed on one side of the aircraft body and is in transmission connection with the first blades through the first driving shaft, and the first blades are uniformly arranged on the periphery of the first driving shaft in the circumferential direction.
Preferably, an infrared distance meter is further disposed below the body to control the flying height.
Preferably, the central control mechanism comprises a display interface, a control key, a status indicator lamp and a PLC, and the display interface, the control key and the status indicator lamp are electrically connected with the PLC.
Preferably, an antenna is further provided inside the body to enable remote control, and the antenna is electrically connected to the PLC.
Preferably, for the convenience of observation, the display interface is a liquid crystal display.
Preferably, the control key is a touch key to enable manual control.
Preferably, the flame retardant rating of the housing is V-0 in order to prevent combustion.
The intelligent unmanned aerial vehicle for wind power generation and seeding has the advantages that the endurance of the unmanned aerial vehicle is improved through the micro power generation mechanism, the unmanned aerial vehicle generates power through the cooperation of the machine body and the second power generation assembly, the use functions of the unmanned aerial vehicle are increased through the seeding mechanism, and the practicability of the unmanned aerial vehicle is improved.
Drawings
The invention is further illustrated with reference to the following figures and examples.
Fig. 1 is a schematic structural diagram of an intelligent unmanned aerial vehicle for wind power generation and capable of sowing of the invention;
fig. 2 is a schematic view of the flying mechanism of the intelligent unmanned aerial vehicle for wind power generation and capable of sowing of the invention;
fig. 3 is a schematic connection diagram of the body of the intelligent unmanned aerial vehicle for wind power generation and seeding and a second power generation assembly;
fig. 4 is a schematic view of a sowing mechanism of the intelligent unmanned aerial vehicle for wind power generation and capable of sowing of the invention;
fig. 5 is a schematic diagram of the switching mechanism of the intelligent unmanned aerial vehicle for wind power generation and capable of sowing of the invention;
in the figure: 1. the intelligent electric seeding machine comprises a machine body, 2 parts of a middle control mechanism, 3 parts of a micro power generation mechanism, 4 parts of a flying mechanism, 5 parts of a first motor, 6 parts of a first driving shaft, 7 parts of a first blade, 8 parts of an infrared range finder, 9 parts of a seeding mechanism, 10 parts of a connecting wire, 11 parts of a moving coil, 12 parts of an electromagnet, 13 parts of a rectifier, 14 parts of a storage battery, 15 parts of a second blade, 16 parts of a first gear, 17 parts of a second driving shaft, 18 parts of a worm, 19 parts of a discharge pipe, 20 parts of a storage box, 21 parts of a stirring paddle, 22 parts of a second motor, 23 parts of a third driving shaft, 24 parts of a first connecting rod, 25 parts of a second connecting rod, 26 parts of a third connecting rod, 27 parts of.
Detailed Description
The present invention will now be described in further detail with reference to the accompanying drawings. These drawings are simplified schematic views illustrating only the basic structure of the present invention in a schematic manner, and thus show only the constitution related to the present invention.
As shown in fig. 1-5, an intelligent unmanned aerial vehicle for wind power generation and capable of sowing comprises a machine body 1, a central control mechanism 2, a micro power generation mechanism 3 and a flight mechanism 4, wherein the central control mechanism 2 is arranged on the machine body 1, the micro power generation mechanism 3 is arranged on the periphery of the machine body 1, the flight mechanism 4 is arranged on two sides of the machine body 1, and the micro power generation mechanism 3 and the flight mechanism 4 are both electrically connected with the central control mechanism 2;
the micro power generation mechanism 3 comprises fan blades, a rotating shaft, a spring and a first power generation assembly, the fan blades are positioned outside the machine body 1 and are uniformly arranged on the periphery of the rotating shaft, one end of the rotating shaft is positioned inside the machine body 1 and is connected with the inner wall of the machine body 1 through the spring, and the rotating shaft is in transmission connection with the first power generation assembly;
a second power generation assembly is arranged below the machine body 1, and the first power generation assembly and the second power generation assembly both comprise power generation units;
the power generation unit comprises a moving coil 11, two electromagnets 12, a rectifier 13 and a storage battery 14, wherein the moving coil 11 is positioned between the two electromagnets 12, the polarities of the two electromagnets 12 are opposite, the moving coil 11 cuts magnetic induction lines of the electromagnets 12 in the moving process, and the moving coil 11 is electrically connected with the storage battery 14 through the rectifier 13;
a connecting wire 10 is arranged below the machine body 1, the machine body 1 is connected with a movable coil 11 of a second power generation assembly through the connecting wire 10, and the rotating shaft is connected with the movable coil 11 of the first power generation assembly;
when needing the electricity generation, first motor 5 starts, it is rotatory to drive first paddle 7, unmanned aerial vehicle takes connecting wire 10 to take off, because the wind power resource of high latitude is very abundant, when unmanned aerial vehicle flies to the take-off height, flight mechanism 4 no longer works, at this moment, unmanned aerial vehicle relies on wind-force to float aloft through connecting wire 10 the same, unmanned aerial vehicle relies on 1 whole body's of organism micro power generation mechanism 3 to carry out wind power generation, supply with self, the duration has been improved, and simultaneously, connecting wire 10 lower extreme and second electricity generation subassembly's removal coil 11 are connected, connecting wire 10 can drive the removal that removes coil 10 was one on the other, at the in-process cutting magnetic induction line production electric current that reciprocates, input battery 14 behind rectifier 13. And, unmanned aerial vehicle detects the height from ground according to infrared distance meter 8, makes unmanned aerial vehicle remain throughout at a relatively stable height.
A seeding mechanism 9 is further arranged below the machine body 1, the seeding mechanism 9 comprises a material storage tank 20, a driving assembly, a stirring assembly and a material discharging pipe 19, the driving assembly is arranged below the machine body 1 and drives the stirring assembly to rotate in the material storage tank 20, the driving assembly comprises a second driving shaft 17, a first gear 16 and a plurality of second blades 15, the second blades 15 are uniformly arranged on the periphery of the second driving shaft 17, and the second driving shaft 17 and the first gear 16 are coaxially arranged;
the stirring assembly comprises a worm 18 and a plurality of stirring paddles 21, the stirring paddles 21 are positioned inside the material storage box 20 and are uniformly arranged on the periphery of the worm 18, and one end of the worm 18 is positioned on one side of the first gear 16 and is matched with the first gear 16;
the discharge pipe 19 is arranged below the material storage tank 20, and a switch mechanism is further arranged inside the material storage tank 20.
When needs sow, start unmanned aerial vehicle, because wind-force, a plurality of second paddle 15 can begin to rotate, and second paddle 15 drives second drive shaft 17 and rotates, also can rotate thereupon with the first gear 16 of the coaxial setting of second drive shaft 17, because first gear 16 and 18 one end of worm match, so worm 18 begins to rotate, drives the stirring rake 21 rotation of the 18 other end of worm, has just so carried out the even stirring to the seed in the storage case 20. At this time, the second motor 22 is started to drive the first connecting rod 24 to rotate, because one end of the second connecting rod 25 is hinged to the other end of the first connecting rod 24, and the other end of the second connecting rod 25 is in transmission connection with the sealing cover 28 through the third connecting rod 26, the third connecting rod 26 realizes horizontal movement through the limiting sleeve 27, and drives the sealing cover 28 to open and close.
Preferably, the opening and closing mechanism comprises a second motor 22, a third driving shaft 23, a first connecting rod 24, a second connecting rod 25, a third connecting rod 26 and a sealing cover 28, the second motor 22 is in transmission connection with the first connecting rod 24 through the third driving shaft 23, one end of the first connecting rod 24 is hinged with the third driving shaft 23, the other end of the first connecting rod 24 is hinged with one end of the second connecting rod 25, the other end of the second connecting rod 25 is in transmission connection with the sealing cover 28 through the third connecting rod 26, and the sealing cover 28 is arranged at the connection position of the storage box 20 and the discharge pipe 19.
Preferably, in order to horizontally move the sealing cover 28, a limiting sleeve 27 is sleeved on the outer periphery of the third connecting rod 26, and the limiting sleeve 27 is fixed inside the storage box 20.
Preferably, the flying mechanism 4 comprises a first motor 5, a first driving shaft 6 and a plurality of first blades 7, the first motor 5 is fixed on one side of the machine body 1, the first motor 5 is in transmission connection with each first blade 7 through the first driving shaft 6, and the first blades 7 are circumferentially and uniformly arranged on the periphery of the first driving shaft 6.
Preferably, an infrared distance meter 8 is further provided below the body 1 in order to control the flying height.
Preferably, the central control mechanism 2 comprises a display interface, a control key, a status indicator lamp and a PLC, and the display interface, the control key and the status indicator lamp are all electrically connected with the PLC.
Preferably, an antenna is further provided inside the machine body 1 to enable remote control, and the antenna is electrically connected to the PLC.
Preferably, for the convenience of observation, the display interface is a liquid crystal display.
Preferably, the control key is a touch key to enable manual control.
Preferably, the flame retardant rating of the body 1 is V-0 in order to prevent combustion.
Compared with the prior art, this an intelligent unmanned aerial vehicle that is arranged in wind power generation and can sow, through miniature power generation mechanism 3, improved unmanned aerial vehicle's duration, through organism 1 and the cooperation of second electricity generation subassembly, realized the unmanned aerial vehicle electricity generation, through sowing mechanism, increased unmanned aerial vehicle's service function, these have all promoted unmanned aerial vehicle's practicality.
In light of the foregoing description of the preferred embodiment of the present invention, many modifications and variations will be apparent to those skilled in the art without departing from the spirit and scope of the invention. The technical scope of the present invention is not limited to the content of the specification, and must be determined according to the scope of the claims.
Claims (10)
1. The intelligent unmanned aerial vehicle is used for wind power generation and can be used for sowing, and is characterized by comprising a machine body (1), a middle control mechanism (2), a micro power generation mechanism (3) and a flight mechanism (4), wherein the middle control mechanism (2) is arranged on the machine body (1), the micro power generation mechanism (3) is arranged on the periphery of the machine body (1), the flight mechanism (4) is arranged on two sides of the machine body (1), and the micro power generation mechanism (3) and the flight mechanism (4) are both electrically connected with the middle control mechanism (2);
the micro power generation mechanism (3) comprises fan blades, a rotating shaft, a spring and a first power generation assembly, the fan blades are positioned outside the machine body (1) and are uniformly arranged on the periphery of the rotating shaft, one end of the rotating shaft is positioned inside the machine body (1) and is connected with the inner wall of the machine body (1) through the spring, and the rotating shaft is in transmission connection with the first power generation assembly;
a second power generation assembly is arranged below the machine body (1), and the first power generation assembly and the second power generation assembly comprise power generation units;
the power generation unit comprises a moving coil (11), two electromagnets (12), a rectifier (13) and a storage battery (14), wherein the moving coil (11) is positioned between the two electromagnets (12), the polarities of the two electromagnets (12) are opposite, the moving coil (11) cuts magnetic induction lines of the electromagnets (12) in the moving process, and the moving coil (11) is electrically connected with the storage battery (14) through the rectifier (13);
a connecting wire (10) is arranged below the machine body (1), the machine body (1) is connected with a moving coil (11) of the second power generation assembly through the connecting wire (10), and the rotating shaft is connected with the moving coil (11) of the first power generation assembly;
a seeding mechanism (9) is further arranged below the machine body (1), the seeding mechanism (9) comprises a storage box (20), a driving assembly, a stirring assembly and a discharge pipe (19), the driving assembly is arranged below the machine body (1) and drives the stirring assembly to rotate in the storage box (20), the driving assembly comprises a second driving shaft (17), a first gear (16) and a plurality of second blades (15), the second blades (15) are uniformly arranged on the periphery of the second driving shaft (17), and the second driving shaft (17) and the first gear (16) are coaxially arranged;
the stirring assembly comprises a worm (18) and a plurality of stirring paddles (21), the stirring paddles (21) are positioned in the material storage box (20) and are uniformly arranged on the periphery of the worm (18), and one end of the worm (18) is positioned on one side of the first gear (16) and is matched with the first gear (16);
the discharging pipe (19) is arranged below the material storage box (20), and a switch mechanism is further arranged inside the material storage box (20).
2. The intelligent unmanned aerial vehicle for wind power generation and seeding is characterized in that the switch mechanism comprises a second motor (22), a third driving shaft (23), a first connecting rod (24), a second connecting rod (25), a third connecting rod (26) and a sealing cover (28), the second motor (22) is in transmission connection with the first connecting rod (24) through the third driving shaft (23), one end of the first connecting rod (24) is hinged with the third driving shaft (23), the other end of the first connecting rod (24) is hinged with one end of the second connecting rod (25), the other end of the second connecting rod (25) is in transmission connection with the sealing cover (28) through the third connecting rod (26), and the sealing cover (28) is arranged at the connection position of the storage box (20) and the discharging pipe (19).
3. The intelligent unmanned aerial vehicle for wind power generation and capable of sowing according to claim 2, wherein a limiting sleeve (27) is sleeved on the periphery of the third connecting rod (26), and the limiting sleeve (27) is fixed inside the storage box (20).
4. The intelligent unmanned aerial vehicle for wind power generation and seeding as claimed in claim 1, wherein the flying mechanism (4) comprises a first motor (5), a first driving shaft (6) and a plurality of first blades (7), the first motor (5) is fixed on one side of the machine body (1), the first motor (5) is in transmission connection with each first blade (7) through the first driving shaft (6), and the first blades (7) are uniformly arranged on the periphery of the first driving shaft (6) in the circumferential direction.
5. The intelligent unmanned aerial vehicle for wind power generation and seeding as claimed in claim 1, wherein an infrared distance meter (8) is further provided below the body (1).
6. The intelligent unmanned aerial vehicle for wind power generation and capable of sowing according to claim 1, wherein the central control mechanism (2) comprises a display interface, control keys, a status indicator light and a PLC, and the display interface, the control keys and the status indicator light are all electrically connected with the PLC.
7. The intelligent unmanned aerial vehicle for wind power generation and capable of sowing according to claim 6, wherein an antenna is further arranged inside the body (1), and the antenna is electrically connected with the PLC.
8. The intelligent unmanned aerial vehicle for wind power generation and capable of sowing of claim 6, wherein the display interface is a liquid crystal display.
9. The intelligent unmanned aerial vehicle for wind power generation and capable of sowing of claim 6, wherein the control button is a touch button.
10. The intelligent drone for wind power generation and capable of sowing according to claim 1, characterized by the flame-retardant rating of the airframe (1) being V-0.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710476592.8A CN107310724B (en) | 2017-06-21 | 2017-06-21 | Intelligent unmanned aerial vehicle used for wind power generation and capable of sowing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710476592.8A CN107310724B (en) | 2017-06-21 | 2017-06-21 | Intelligent unmanned aerial vehicle used for wind power generation and capable of sowing |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107310724A CN107310724A (en) | 2017-11-03 |
| CN107310724B true CN107310724B (en) | 2020-02-21 |
Family
ID=60182023
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710476592.8A Expired - Fee Related CN107310724B (en) | 2017-06-21 | 2017-06-21 | Intelligent unmanned aerial vehicle used for wind power generation and capable of sowing |
Country Status (1)
| Country | Link |
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| CN (1) | CN107310724B (en) |
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| CN111955828A (en) * | 2020-08-21 | 2020-11-20 | 国网山东省电力公司莱芜供电公司 | Wind-force spontaneous heating gloves |
| CN113092190B (en) * | 2021-03-17 | 2024-02-06 | 陕西国臻实业集团有限公司 | Atmospheric pollution monitoring sampling device based on unmanned aerial vehicle remote control |
| CN113060286A (en) * | 2021-04-29 | 2021-07-02 | 宣城宣美文化发展有限公司 | Agricultural plant protection unmanned aerial vehicle that can spray by a large scale |
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| CN104494829A (en) * | 2014-11-19 | 2015-04-08 | 成都群侠科技有限公司 | Low-altitude seeding unmanned aerial vehicle |
| CN205311910U (en) * | 2015-11-24 | 2016-06-15 | 无锡觅睿恪科技有限公司 | Agriculture unmanned aerial vehicle that can evenly sow seeds |
| CN106143908A (en) * | 2016-07-06 | 2016-11-23 | 陈嘉玲 | A kind of safe and reliable Intelligent unattended machine with online generating function |
| CN106314806A (en) * | 2016-10-19 | 2017-01-11 | 黄河交通学院 | Wind-solar complementary generation system of UAV (unmanned aerial vehicle) and operation method of system |
| CN106628159A (en) * | 2016-09-22 | 2017-05-10 | 广州市婵昕生物科技有限责任公司 | Unmanned plane based on Internet of Things and used for agricultural production |
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| US8579234B2 (en) * | 2011-04-01 | 2013-11-12 | Texas Transland LLC | System and method for affixing gateboxes to an aircraft |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104494829A (en) * | 2014-11-19 | 2015-04-08 | 成都群侠科技有限公司 | Low-altitude seeding unmanned aerial vehicle |
| CN205311910U (en) * | 2015-11-24 | 2016-06-15 | 无锡觅睿恪科技有限公司 | Agriculture unmanned aerial vehicle that can evenly sow seeds |
| CN106143908A (en) * | 2016-07-06 | 2016-11-23 | 陈嘉玲 | A kind of safe and reliable Intelligent unattended machine with online generating function |
| CN106628159A (en) * | 2016-09-22 | 2017-05-10 | 广州市婵昕生物科技有限责任公司 | Unmanned plane based on Internet of Things and used for agricultural production |
| CN106314806A (en) * | 2016-10-19 | 2017-01-11 | 黄河交通学院 | Wind-solar complementary generation system of UAV (unmanned aerial vehicle) and operation method of system |
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