CN117799889B - Charging equipment for unmanned aerial vehicle and charging method thereof - Google Patents
Charging equipment for unmanned aerial vehicle and charging method thereof Download PDFInfo
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- CN117799889B CN117799889B CN202410224792.4A CN202410224792A CN117799889B CN 117799889 B CN117799889 B CN 117799889B CN 202410224792 A CN202410224792 A CN 202410224792A CN 117799889 B CN117799889 B CN 117799889B
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- 238000000034 method Methods 0.000 title claims abstract description 9
- 239000000872 buffer Substances 0.000 claims abstract description 21
- 238000007789 sealing Methods 0.000 claims abstract description 19
- 230000003139 buffering effect Effects 0.000 claims abstract description 17
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 9
- 230000005291 magnetic effect Effects 0.000 claims description 7
- 230000001360 synchronised effect Effects 0.000 claims description 7
- 239000000428 dust Substances 0.000 claims description 6
- 230000017525 heat dissipation Effects 0.000 claims description 6
- 235000017166 Bambusa arundinacea Nutrition 0.000 claims description 3
- 235000017491 Bambusa tulda Nutrition 0.000 claims description 3
- 241001330002 Bambuseae Species 0.000 claims description 3
- 235000015334 Phyllostachys viridis Nutrition 0.000 claims description 3
- 239000011425 bamboo Substances 0.000 claims description 3
- 229910052799 carbon Inorganic materials 0.000 claims description 3
- 239000003381 stabilizer Substances 0.000 claims description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Chemical compound O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 2
- 238000001816 cooling Methods 0.000 claims 1
- 238000004140 cleaning Methods 0.000 abstract description 8
- 238000010586 diagram Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 230000000087 stabilizing effect Effects 0.000 description 3
- 208000035473 Communicable disease Diseases 0.000 description 1
- 241000196324 Embryophyta Species 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 239000003302 ferromagnetic material Substances 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 239000004576 sand Substances 0.000 description 1
Classifications
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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
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
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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
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
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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
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/14—Plug-in electric vehicles
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- Electric Propulsion And Braking For Vehicles (AREA)
Abstract
The invention relates to the technical field of unmanned aerial vehicle charging, and discloses charging equipment and a charging method thereof for an unmanned aerial vehicle, wherein the charging equipment comprises a charging fixing seat, one side of the top end of the charging fixing seat is fixedly connected with a charging fixing block, the side surface of the charging fixing block is fixedly connected with a sealing box, the inside of the sealing box is fixedly connected with a charging plug, one side of the top end of the charging fixing seat far away from the charging fixing block is fixedly connected with a buffer mechanism, and the bottom end of the buffer mechanism is movably connected with a cleaning and radiating mechanism; according to the invention, the shutdown plate, the connecting rod, the square and the side buffering component are arranged, so that the unmanned aerial vehicle falls on the shutdown plate, and the shutdown plate moves downwards and drives the square to move downwards along with the falling of the unmanned aerial vehicle, so that the main spring is compressed for buffering, and the movement of the shutdown plate in the horizontal direction is buffered through the side buffering component on the side surface of the square, so that the unmanned aerial vehicle can be buffered in the vertical and horizontal directions, and the damage of the unmanned aerial vehicle is avoided.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicle charging, in particular to charging equipment for an unmanned aerial vehicle and a charging method thereof.
Background
Unmanned plane is called unmanned plane for short, unmanned plane is unmanned plane that utilizes radio remote control equipment and self-contained program control device to operate, or operate independently by on-vehicle computer totally or intermittently, compared with unmanned plane, unmanned plane is more suitable for the task that is too "fooled, dirty or dangerous", unmanned plane has very wide application in fields such as taking photo by plane, agriculture, plant protection, miniature self-timer, express delivery transportation, disaster relief, observing wild animal, monitoring infectious disease, mapping, news report, etc.;
When charging, the unmanned aerial vehicle needs to be fixed at first, after a charging wire is connected with a charging port of the unmanned aerial vehicle, the unmanned aerial vehicle is charged, and the unmanned aerial vehicle is charged in a dry, moisture-free and dust-free place, and the external windy state is avoided during charging, so that dust and sand are prevented from entering a battery or a charger, the charging effect and the service life of the battery are influenced, but the existing unmanned aerial vehicle charging equipment has the following problems:
When the unmanned aerial vehicle needs to be charged, the unmanned aerial vehicle needs to land on the charging equipment, when the unmanned aerial vehicle lands, the unmanned aerial vehicle directly contacts with the charging equipment, and the unmanned aerial vehicle is possibly damaged, and when the unmanned aerial vehicle lands, the unmanned aerial vehicle can also slightly move in the horizontal direction except the movement in the vertical direction, the traditional charging equipment cannot buffer in multiple directions, and cannot well protect the unmanned aerial vehicle;
When unmanned aerial vehicle is in use, it is in external environment always, probably has dust or steam in unmanned aerial vehicle's the interface that charges, if directly is connected charging plug and the interior interface of unmanned aerial vehicle this moment, probably has the condition of electric leakage, can cause the damage to equipment to when unmanned aerial vehicle is charging, equipment self temperature is higher this moment, needs in time to cool down the processing.
Disclosure of Invention
In order to overcome the above-mentioned drawbacks of the prior art, embodiments of the present invention provide a charging device for an unmanned aerial vehicle and a charging method thereof, so as to solve the technical problems set forth in the background art.
In order to achieve the above purpose, the present invention provides the following technical solutions: the charging equipment for the unmanned aerial vehicle and the charging method thereof comprise a charging fixing seat, wherein one side of the top end of the charging fixing seat is fixedly connected with a charging fixing block, the side surface of the charging fixing block is fixedly connected with a sealing box, the inside of the sealing box is fixedly connected with a charging plug, one side of the top end of the charging fixing seat, which is far away from the charging fixing block, is fixedly connected with a buffer mechanism, the bottom end of the buffer mechanism is movably connected with a cleaning and heat dissipation mechanism, and the unmanned aerial vehicle is placed at the top end of the buffer mechanism; the buffer gear includes the shut down board that contacts with unmanned aerial vehicle, the bottom fixedly connected with connecting rod of shut down board, the bottom fixedly connected with square of connecting rod, the equal fixedly connected with side of four sides of square is slowed down the subassembly, the bottom fixedly connected with movable rod of connecting rod, the side swing joint of square has the fly leaf, the side of movable rod is equipped with the main spring, the main spring is located the top of fly leaf, the side swing joint of fly leaf has the spread box, the spout that can supply the fly leaf to remove is seted up to the bottom of spread box.
In a preferred embodiment, the bottom end fixedly connected with of link box keeps away the position piece, keep away the position hole that can supply the movable rod to remove is seted up on the top of position piece, the top of link box has been seted up and has been supplied the connecting rod to carry out the position hole of keeping away that removes, the bottom of link box and the top fixed connection of movable plate.
In a preferred embodiment, the four corners on the top end of the connecting box are fixedly connected with electromagnets, the side surface, close to the sealing box, of the connecting box is fixedly connected with a limiting frame, the side surface, far away from the sealing box, of the connecting box is fixedly connected with a chute, the top end of the limiting frame is provided with a chute, and when the shutdown plate is in contact with the connecting box, the bottom end of the unmanned aerial vehicle is located below the chute of the limiting frame.
In a preferred embodiment, the side fixedly connected with first spherical block of square, the side is slowed down the subassembly and is included first spherical block, the side swing joint that square was kept away from to first spherical block has first hemisphere ring, the side fixedly connected with gag lever post of first hemisphere ring is kept away from to first hemisphere ring, the side fixedly connected with limiting plate that first hemisphere ring was kept away from to the gag lever post, the side swing joint of limiting plate has the connecting cylinder, the side that the limiting plate is close to first hemisphere ring is equipped with the side spring.
In a preferred embodiment, the side spring is located the side of gag lever post, and gag lever post and limiting plate all are located the inside of connecting cylinder, the side fixedly connected with second hemisphere ring of gag lever post is kept away from to the connecting cylinder, the side swing joint that the connecting cylinder was kept away from to the second hemisphere ring has the second spherical piece, the side and the inside fixed connection of link box of second hemisphere ring are kept away from to the second spherical piece.
In a preferred embodiment, the cleaning and heat dissipating mechanism comprises a moving plate, the middle part of the inner side of the moving plate is movably connected with a reciprocating screw rod, two ends of the side surface of the moving plate are movably connected with stabilizing rods, the side surface of the reciprocating screw rod, which is far away from the moving plate, is fixedly connected with a connecting ratchet wheel, the side surface of the connecting ratchet wheel is movably connected with a ratchet wheel sleeve, the side surface of the ratchet wheel sleeve, which is far away from the reciprocating screw rod, is fixedly connected with an output shaft, and the side surface of the output shaft, which is far away from the ratchet wheel sleeve, is fixedly connected with a servo motor.
In a preferred embodiment, the side of the output shaft is fixedly connected with a synchronous wheel, the side of the synchronous wheel is meshed with a synchronous belt, the inside of the top end of the synchronous belt is fixedly connected with a rotating shaft, and the side of the rotating shaft is fixedly connected with a rotating blade.
In a preferred embodiment, the side of the rotating blade, which is close to the sealing box, is provided with a conical cylinder, the side of the conical cylinder, which is far away from the rotating blade, is fixedly connected with an air outlet pipe, the side of the air outlet pipe is fixedly connected with the inside of the sealing box, the side of the rotating blade, which is far away from the sealing box, is provided with an activated carbon plate, and the activated carbon plate is positioned in an air exhaust hole of the charging fixing block.
The invention has the technical effects and advantages that:
According to the invention, the shutdown plate, the connecting rod, the square and the side buffering component are arranged, so that the unmanned aerial vehicle falls on the shutdown plate, and the shutdown plate moves downwards and drives the square to move downwards along with the falling of the unmanned aerial vehicle, so that the main spring is compressed for buffering, and the movement of the shutdown plate in the horizontal direction is buffered through the side buffering component on the side surface of the square, so that the unmanned aerial vehicle can be buffered in the vertical and horizontal directions, and the damage of the unmanned aerial vehicle is avoided;
when the unmanned aerial vehicle falls on the stop plate, at the moment, magnetic repulsion force is generated between the forward energization of the electromagnet and the stop plate, the pressure of the unmanned aerial vehicle during descending is further buffered, the unmanned aerial vehicle is prevented from being damaged by contact with the limit frame or the connecting box due to too fast descending, after the unmanned aerial vehicle is stabilized, the electromagnet is energized reversely, the stop plate drives the electromagnet to move downwards, at the moment, the base of the unmanned aerial vehicle enters the limit frame, and the position of the unmanned aerial vehicle is fixed, so that the unmanned aerial vehicle can accurately contact with the charging plug;
After the unmanned aerial vehicle is fixed, the servo motor controls the output shaft to drive the reciprocating screw rod to rotate through the ratchet sleeve and the connecting ratchet when in forward rotation, the moving plate moves when the stabilizing rod rotates, so that the limiting frame moves to convey the unmanned aerial vehicle to the charging plug for charging, the rotating blade is driven to rotate to blow air into the air outlet pipe when in forward rotation of the output shaft, the air outlet pipe blows out dust and water vapor at the charging port of the unmanned aerial vehicle, when the servo motor controls the output shaft to rotate reversely, the rotating blade is pumped at the moment to cool, the ratchet sleeve is separated from the connecting ratchet when in reverse rotation, and the unmanned aerial vehicle keeps temperature.
Drawings
Fig. 1 is a schematic view of the overall internal structure of the present invention.
Fig. 2 is a schematic diagram of the overall side structure of the interior of the present invention.
Fig. 3 is a schematic overall structure of the present invention.
Fig. 4 is a schematic structural view of a buffering mechanism according to the present invention.
Fig. 5 is a schematic view of the internal structure of the buffering mechanism of the present invention.
Fig. 6 is a schematic diagram of a side buffering assembly according to the present invention.
Fig. 7 is a schematic structural diagram of a cleaning and heat dissipating mechanism according to the present invention.
Fig. 8 is a schematic diagram of a connection structure of a cleaning and heat dissipating mechanism according to the present invention.
The reference numerals are: 1. a charging holder; 2. a charging fixed block; 3. a seal box; 4. unmanned plane; 5. a buffer mechanism; 501. a stop plate; 502. a connecting rod; 503. a square block; 504. a movable rod; 505. a side relief assembly; 5051. a first spherical mass; 5052. a first hemispherical ring; 5053. a limit rod; 5054. a limiting plate; 5055. a side spring; 5056. a connecting cylinder; 5057. a second hemispherical ring; 5058. a second spherical mass; 506. a movable plate; 507. a main spring; 508. a connection box; 509. an electromagnet; 510. a limit frame; 511. a avoidance block; 6. cleaning a heat dissipation mechanism; 601. a moving plate; 602. a stabilizer bar; 603. a reciprocating screw rod; 604. a connecting ratchet wheel; 605. a ratchet sleeve; 606. an output shaft; 607. a servo motor; 608. a synchronizing wheel; 609. a synchronous belt; 610. a rotating shaft; 611. rotating the blade; 612. a conical cylinder; 613. an air outlet pipe; 7. an activated carbon plate; 8. and a charging plug.
Detailed Description
The embodiments of the present invention will be clearly and completely described below with reference to the drawings in the present invention, and the configurations of the structures described in the following embodiments are merely examples, and a charging device for an unmanned aerial vehicle and a charging method thereof according to the present invention are not limited to the structures described in the following embodiments, and all other embodiments obtained by a person having ordinary skill in the art without making any creative effort are within the scope of the present invention.
Referring to fig. 1,2 and 3, the invention provides a charging device for an unmanned aerial vehicle and a charging method thereof, comprising a charging fixing seat 1, wherein one side of the top end of the charging fixing seat 1 is fixedly connected with a charging fixing block 2, the side surface of the charging fixing block 2 is fixedly connected with a sealing box 3, the inside of the sealing box 3 is fixedly connected with a charging plug 8, one side of the top end of the charging fixing seat 1 far away from the charging fixing block 2 is fixedly connected with a buffer mechanism 5, the bottom end of the buffer mechanism 5 is movably connected with a cleaning and heat dissipation mechanism 6, and the top end of the buffer mechanism 5 is provided with the unmanned aerial vehicle 4.
Referring to fig. 3, fig. 4 and fig. 5, buffer gear 5 includes the shut down board 501 that contacts with unmanned aerial vehicle 4, the bottom fixedly connected with connecting rod 502 of shut down board 501, the bottom fixedly connected with square 503 of connecting rod 502, four equal fixedly connected with side buffering subassembly 505 of side of square 503, the bottom fixedly connected with movable rod 504 of connecting rod 502, the side swing joint of square 503 has movable board 506, the side of movable rod 504 is equipped with main spring 507, main spring 507 is located the top of movable board 506, the side swing joint of movable board 506 has the spread box 508, the spout that can supply movable board 506 to remove is seted up to the bottom of spread box 508, the bottom fixedly connected with of spread box 508 keeps away from position piece 511, the top of keeping away position piece 511 has been seted up and has been supplied movable rod 504 to move keep away from the position hole, the top of spread box 508 has been seted up and can supply connecting rod 502 to move keep away from position hole, the bottom of spread box 508 and the top fixedly connected with movable plate 601, the four corners on top of spread box 508 all fixedly connected with electro-magnet 509, the side of spread box 508 is close to the side of sealed box 3 and keeps away from the side of movable plate 506 and the top of movable plate 506, the side of spread box 508 is close to the side sealed box 510 and keeps away from the top of the sealed box 3 has the top 510, the top of spread box 510 is located down with the spout of the sealed box 510, the side of the top is located down with the top of the sealed box 510, and is located down in the position of the position-limited frame of the unmanned aerial vehicle is located under the top is located down by the top has been separated position of the top has been separated by the top has.
In the embodiment of the application, when the unmanned aerial vehicle 4 falls on the shutdown plate 501, the impact force in the vertical direction can be buffered by the compression of the main spring 507, the buffer effect is achieved, the connecting box 508 is provided with the clearance hole, so that no collision is generated when the shutdown plate 501 shakes in the horizontal direction, the movable plate 506 moves in the sliding groove at the bottom end of the connecting box 508, and the movable rod 504 can move up and down in the movable plate 506 when the movable plate 506 moves in the sliding groove, so that the mutual collision or clamping condition can not occur when the application buffers in different directions, the limiting frame 510 is arranged on the connecting box 508, and magnetic repulsive force can be generated between the electromagnet 509 and the connecting box 508 when the electromagnet 509 is electrified in the forward direction, the connection box 508 is made of ferromagnetic material, and is buffered at this time, after the unmanned aerial vehicle 4 is stabilized, the electromagnet 509 is electrified reversely at this time to generate magnetic attraction with the shutdown plate 501, so that the connection box 508 can be in contact with the shutdown plate 501, and because the lower part of the unmanned aerial vehicle 4 is positioned below the chute of the limit frame 510, the unmanned aerial vehicle 4 can be driven to move when the limit frame 510 moves, the chute is arranged above the limit frame 510, so that the shutdown plate 501 cannot be in contact with the limit frame 510 when the shutdown plate 501 swings in the horizontal direction in the initial stage, and larger swing is avoided.
Referring to fig. 5 and6, the side surface of the square 503 is fixedly connected with a first ball 5051, the side buffering component 505 comprises the first ball 5051, the side surface of the first ball 5051, which is far away from the square 503, is movably connected with a first hemispherical ring 5052, the side surface of the first hemispherical ring 5052, which is far away from the first ball 5051, is fixedly connected with a limit plate 5053, the side surface of the limit plate 5054, which is movably connected with a connecting barrel 5056, the side surface of the limit plate 5054, which is near to the first hemispherical ring 5052, is provided with a side spring 5055, the side spring 5055 is located on the side surface of the limit rod 5053, the limit rod 5053 and the limit plate 5054 are both located inside the connecting barrel 5056, the side surface of the connecting barrel 5056, which is far away from the limit rod 5053, is fixedly connected with a second hemispherical ring 5057, the side surface of the second hemispherical ring 5057, which is far away from the connecting barrel 5056, is movably connected with a second spherical block 5058, and the side surface of the second hemispherical ring 5058 is far away from the second hemispherical ring 5057 is fixedly connected with the inside of the connecting box 508.
In the embodiment of the application, when the unmanned aerial vehicle 4 drives the stop plate 501 to rotate in the horizontal direction, the square 503 moves in the horizontal direction, the limit rod 5053 drives the connecting cylinder 5056 to move when the square 503 moves, the side spring 5055 is compressed when the square is moved, the first spherical block 5051 can rotate in the first hemispherical ring 5052, and the second spherical block 5058 can rotate in the second hemispherical ring 5057, so that the limit rod 5053 can stably move when the limit rod 5053 moves vertically upwards, and the stability of the unmanned aerial vehicle is ensured when the unmanned aerial vehicle is buffered, and in addition, the application needs to be explained, when the unmanned aerial vehicle 4 moves leftwards, the left side spring 5055 is compressed and plays a role in buffering.
Referring to fig. 2, fig. 5, fig. 7 and fig. 8, the cleaning and heat dissipation mechanism 6 comprises a moving plate 601, a reciprocating screw rod 603 is movably connected to the middle of the inner side of the moving plate 601, two ends of the side surface of the moving plate 601 are movably connected with a stabilizing rod 602, the side surface of the reciprocating screw rod 603, which is far away from the moving plate 601, is fixedly connected with a connecting ratchet 604, the side surface of the connecting ratchet 604 is movably connected with a ratchet sleeve 605, the side surface of the ratchet sleeve 605, which is far away from the reciprocating screw rod 603, is fixedly connected with an output shaft 606, the side surface of the output shaft 606 is far away from the ratchet sleeve 605, is fixedly connected with a servo motor 607, the side surface of the output shaft 606 is fixedly connected with a synchronizing wheel 608, the side surface of the synchronizing wheel 608 is meshed with a synchronizing belt 609, the inner part of the top end of the synchronizing belt 609 is fixedly connected with a rotating shaft 610, the side surface of the rotating shaft 610 is fixedly connected with a rotating blade 611, the side surface of the rotating blade 611 is near to the side surface of the sealing box 3 is provided with a conical cylinder 612, the side surface of the conical cylinder 612 is far away from the rotating blade 611 is fixedly connected with an air outlet tube 613, the side surface of the air outlet tube 613, the side of the rotating blade is fixedly connected with the inner fixedly connected with a sealing box 3, the side surface of the rotating blade 7 is far away from the rotating blade 3, the side of the rotating blade 3 is located in the exhaust hole of the charging fixing block 2.
In the embodiment of the application, because of the connection relationship between the connection ratchet 604 and the ratchet sleeve 605, when the servo motor 607 drives the output shaft 606 and the ratchet sleeve 605 to rotate forward, the ratchet sleeve 605 can drive the connection ratchet 604 to rotate at the moment, when the servo motor 607 rotates reversely, the reverse ratchet sleeve 605 cannot drive the connection ratchet 604 to rotate, when the output shaft 606 rotates forward, the rotating blade 611 rotates forward, external air is blown into the conical cylinder 612, the air is dehumidified by the active carbon plate 7, the air enters the conical cylinder 612 and accelerates, the air is discharged from the air outlet pipe 613 and blown into the charging port of the unmanned aerial vehicle 4, dust and vapor in the charging port are blown out, and when the reciprocating screw 603 rotates, the moving plate 601 moves reciprocally, so that when the moving plate 601 moves to the side closest to the sealing box 3, the unmanned aerial vehicle 4 is sent to the sealing box 3 and the charging plug 8, and after the servo motor 611 rotates forward again, the moving plate 601 moves reversely, so that the unmanned aerial vehicle 4 is connected with the charging plug 8, the rotating blade 607 is controlled to take off, and the unmanned aerial vehicle 4 can be directly cooled when the output shaft 607 rotates, and the unmanned aerial vehicle 4 is not cooled.
The working principle of the invention is as follows: the unmanned aerial vehicle 4 falls above the shutdown plate 501, when the unmanned aerial vehicle 4 contacts with the shutdown plate 501, the shutdown plate 501 moves downwards at the moment, the shutdown plate 501 moves downwards through the connecting rod 502, the block 503 compresses the main spring 507 when moving downwards to buffer in the vertical direction, when the unmanned aerial vehicle 4 drives the shutdown plate 501 to move in the horizontal direction, the block 503 moves horizontally at the moment, the block 503 moves horizontally to drive the first spherical block 5051 to move, the first spherical block 5051 rotates in the first hemispherical ring 5052 and drives the first hemispherical ring 5052 to move, and at the moment, the first hemispherical ring 5052 drives the limiting plate 5054 to move through the limiting rod 5053 and compress the side buffering component 505 to buffer in the horizontal direction;
when the unmanned aerial vehicle 4 lands, the electromagnet 509 is electrified forward and generates magnetic repulsion force with the stop plate 501, when the unmanned aerial vehicle 4 is stable, the electromagnet 509 is electrified reversely and generates magnetic attraction force with the stop plate 501, and the stop plate 501 and the unmanned aerial vehicle 4 above the stop plate move downwards together and enter into limit grooves at the bottom ends of the two limit frames 510 to fix the unmanned aerial vehicle 4;
When the unmanned aerial vehicle 4 is fixed, servo motor 607 controls output shaft 606 to positively rotate, can drive when output shaft 606 drives ratchet sleeve 605 positively and connect ratchet 604 rotation, drive reciprocal lead screw 603 rotation when connecting ratchet 604 rotates, and make movable plate 601 remove, when spacing frame 510 moves to the position that is closest to seal box 3, unmanned aerial vehicle 4 is connected with charging plug 8 and charges, when output shaft 606 positively rotates, drive axis of rotation 610 through synchronizing wheel 608 and synchronizing wheel 608, then make rotor blade 611 positively rotate and blow in toper section of thick bamboo 612 and outlet duct 613, the dust and the steam blowing in the side that the gas blown to unmanned aerial vehicle 4 through outlet duct 613 in with its mouth that charges fall, when unmanned aerial vehicle 4 charges, servo motor 607 controls output shaft 606 reversal, can't drive connection ratchet 604 rotation through ratchet sleeve 605 when output shaft 606 reversal, output shaft 606 reversal makes rotor blade 611 reversal with the gas blow out, cool down to unmanned aerial vehicle 4 that charges, servo motor 607 drives output shaft 606 again positively and rotates, make reciprocal lead screw 603 rotate, make reciprocating lead screw 603 rotate, make when output shaft 603 rotates, make unmanned aerial vehicle 510 take out from the position that is closest to seal box 3 when sealing box 4 is charged, take out after unmanned aerial vehicle 4 is kept away from seal box.
Finally: the foregoing is only illustrative of the preferred embodiments of the present invention and is not to be construed as limiting the invention, but rather as various modifications, equivalent arrangements, improvements, etc., within the spirit and principles of the present invention.
Claims (6)
1. Charging equipment for unmanned aerial vehicle, including charging fixing base (1), its characterized in that: one side fixedly connected with that charges fixing base (1) top charges fixed block (2), the side fixedly connected with seal box (3) that charges fixed block (2), the inside fixedly connected with of seal box (3) charges plug (8), one side fixedly connected with buffer gear (5) that charges fixing base (1) top kept away from charging fixed block (2), the bottom swing joint of buffer gear (5) has clean heat dissipation mechanism (6), unmanned aerial vehicle (4) have been placed on the top of buffer gear (5); the buffer mechanism (5) comprises a stop plate (501) which is in contact with the unmanned aerial vehicle (4), a connecting rod (502) is fixedly connected to the bottom end of the stop plate (501), a square block (503) is fixedly connected to the bottom end of the connecting rod (502), side buffering components (505) are fixedly connected to four sides of the square block (503), a movable rod (504) is fixedly connected to the bottom end of the connecting rod (502), a movable plate (506) is movably connected to the side of the square block (503), a main spring (507) is arranged on the side of the movable rod (504), the main spring (507) is located at the top end of the movable plate (506), a connecting box (508) is movably connected to the side of the movable plate (506), and a chute capable of being used for moving the movable plate (506) is formed in the bottom end of the connecting box (508);
The bottom end of the connecting box (508) is fixedly connected with a avoidance block (511), the top end of the avoidance block (511) is provided with a avoidance hole for the movable rod (504) to move, the top end of the connecting box (508) is provided with a avoidance hole for the connecting rod (502) to move, and the bottom end of the connecting box (508) is fixedly connected with the top end of the moving plate (601);
The four corners at the top end of the connecting box (508) are fixedly connected with electromagnets (509), the side surface, close to the sealing box (3), of the connecting box (508) and the side surface, far away from the sealing box (3) are fixedly connected with limiting frames (510), the top end of each limiting frame (510) is provided with a chute, and when the shutdown plate (501) is in contact with the connecting box (508), the bottom end of the unmanned aerial vehicle (4) is positioned below the chute of each limiting frame (510);
A charging method comprising the steps of:
Step S1, when the unmanned aerial vehicle (4) falls above the shutdown plate (501), the shutdown plate (501) moves downwards at the moment when the unmanned aerial vehicle (4) contacts with the shutdown plate (501), the shutdown plate (501) drives the square block (503) to move downwards through the connecting rod (502) when moving downwards, the main spring (507) is compressed when the square block (503) moves downwards, buffering is carried out in the vertical direction, when the unmanned aerial vehicle (4) drives the shutdown plate (501) to move in the horizontal direction, the square block (503) moves horizontally at the moment, the square block (503) moves horizontally to drive the first spherical block (5051) to move, the first spherical block (5051) rotates in the first hemispherical ring (5052) and drives the first hemispherical ring (5052) to move, and the first hemispherical ring (5052) drives the limiting plate (5054) to move through the limiting rod (5053) and compresses the side buffering component (505) to buffer in the horizontal direction;
S2, when the unmanned aerial vehicle (4) falls, the electromagnet (509) is electrified forward and generates magnetic repulsion force with the stop plate (501), after the unmanned aerial vehicle (4) is stable, the electromagnet (509) is electrified reversely and generates magnetic attraction force with the stop plate (501), and the stop plate (501) and the unmanned aerial vehicle (4) above the stop plate move downwards together and enter into limit grooves at the bottom ends of the two limit frames (510), so that the unmanned aerial vehicle (4) is fixed;
Step S3, when the unmanned aerial vehicle (4) is fixed, the servo motor (607) controls the output shaft (606) to rotate positively, the output shaft (606) drives the ratchet sleeve (605) to rotate positively and can drive the connecting ratchet (604) to rotate, the connecting ratchet (604) drives the reciprocating screw rod (603) to rotate and enables the moving plate (601) to move, when the moving plate (601) moves to the position closest to the sealing box (3) through the limiting frame (510), the unmanned aerial vehicle (4) is connected with the charging plug (8) to charge, when the output shaft (606) rotates positively, the synchronous wheel (608) and the synchronous wheel (608) drive the rotating shaft (610) to rotate, then the rotating blade (611) rotates positively and blows air into the conical barrel (612) and the air outlet pipe (613), and air blows dust and water vapor in a charging port of the unmanned aerial vehicle (4) to the side surface through the air outlet pipe (613);
Step S4 unmanned aerial vehicle (4) when charging, servo motor (607) control output shaft (606) are in reverse rotation, can't drive through ratchet sleeve (605) when output shaft (606) are in reverse rotation and connect ratchet (604) and rotate, output shaft (606) are in reverse rotation and make rotor blade (611) reverse rotation, rotor blade (611) blows out gas, unmanned aerial vehicle (4) cooling to charging, after charging, servo motor (607) drive output shaft (606) forward rotation again, make reciprocating screw (603) rotate when output shaft (606) forward rotation, reciprocating screw (603) make spacing frame (510) keep away from seal box (3) from the position that is closest to seal box (3) and remove unmanned aerial vehicle (4) after charging.
2. A charging device for an unmanned aerial vehicle according to claim 1, wherein: the side fixedly connected with first ball piece (5051) of square (503), side buffering subassembly (505) is including first ball piece (5051), the side swing joint that square (503) was kept away from to first ball piece (5051) has first hemisphere ring (5052), the side fixedly connected with gag lever post (5053) of first hemisphere piece (5052) is kept away from to first hemisphere ring (5052), the side fixedly connected with limiting plate (5054) of first hemisphere ring (5052) is kept away from to gag lever post (5053), the side swing joint of limiting plate (5054) has connecting cylinder (5056), the side that limiting plate (5054) is close to first hemisphere ring (5052) is equipped with side spring (5055).
3. A charging device for an unmanned aerial vehicle according to claim 2, wherein: side spring (5055) are located the side of gag lever post (5053), and gag lever post (5053) and limiting plate (5054) all are located the inside of connecting cylinder (5056), the side fixedly connected with second hemisphere ring (5057) of gag lever post (5053) are kept away from to connecting cylinder (5056), the side swing joint that connecting cylinder (5056) was kept away from to second hemisphere ring (5057) has second ball (5058), the side and the inside fixed connection of junction box (508) of second hemisphere ring (5057) are kept away from to second ball (5058).
4. A charging device for an unmanned aerial vehicle according to claim 1, wherein: clean heat dissipation mechanism (6) including movable plate (601), the inboard middle part swing joint of movable plate (601) has reciprocating lead screw (603), the both ends swing joint of movable plate (601) side has stabilizer bar (602), the side fixedly connected with connection ratchet (604) of movable plate (601) are kept away from to reciprocating lead screw (603), the side swing joint of connection ratchet (604) has ratchet sleeve (605), the side fixedly connected with output shaft (606) of reciprocating lead screw (603) are kept away from to ratchet sleeve (605), the side fixedly connected with servo motor (607) of ratchet sleeve (605) are kept away from to output shaft (606).
5. A charging device for an unmanned aerial vehicle as claimed in claim 4, wherein: the side fixedly connected with synchronizing wheel (608) of output shaft (606), the side meshing of synchronizing wheel (608) has hold-in range (609), the inside fixedly connected with axis of rotation (610) on hold-in range (609) top, the side fixedly connected with turning vane (611) of axis of rotation (610).
6. A charging device for an unmanned aerial vehicle according to claim 5, wherein: the side that rotor blade (611) is close to seal box (3) is equipped with toper section of thick bamboo (612), the side fixedly connected with outlet duct (613) of rotor blade (611) are kept away from to toper section of thick bamboo (612), the side and the inside fixed connection of seal box (3) of outlet duct (613), the side that rotor blade (611) kept away from seal box (3) is equipped with active carbon plate (7), active carbon plate (7) are located the exhaust hole of charging fixed block (2).
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