CN214986136U - Automatic four rotor unmanned aerial vehicle who changes receive and release system - Google Patents
Automatic four rotor unmanned aerial vehicle who changes receive and release system Download PDFInfo
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- CN214986136U CN214986136U CN202120366078.0U CN202120366078U CN214986136U CN 214986136 U CN214986136 U CN 214986136U CN 202120366078 U CN202120366078 U CN 202120366078U CN 214986136 U CN214986136 U CN 214986136U
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- 238000004891 communication Methods 0.000 claims abstract description 19
- 238000005516 engineering process Methods 0.000 claims abstract description 9
- 238000012544 monitoring process Methods 0.000 claims description 97
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical group [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 24
- 239000002184 metal Substances 0.000 claims description 24
- 229910052751 metal Inorganic materials 0.000 claims description 24
- 229910052802 copper Inorganic materials 0.000 claims description 13
- 239000010949 copper Substances 0.000 claims description 13
- 239000000523 sample Substances 0.000 claims description 12
- 230000000994 depressogenic effect Effects 0.000 claims description 6
- 230000005611 electricity Effects 0.000 claims description 3
- 238000012423 maintenance Methods 0.000 abstract description 16
- 238000000034 method Methods 0.000 description 10
- 238000011084 recovery Methods 0.000 description 8
- 238000010586 diagram Methods 0.000 description 3
- 230000004087 circulation Effects 0.000 description 2
- 238000005192 partition Methods 0.000 description 1
- 238000001179 sorption measurement Methods 0.000 description 1
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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
- Y02T90/12—Electric charging stations
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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
- Y02T90/16—Information or communication technologies improving the operation of electric vehicles
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Abstract
The utility model discloses an automatic four rotor unmanned aerial vehicle receive and release system who changes, including the hangar, the support column, the arm, four rotor unmanned aerial vehicle, a control system, A rotary device, B rotary device and C rotary device, the support column sets up at the hangar middle part, the outer wall of support column is D1 with the distance of hangar, the one end of arm is passed through A rotary device and is connected with the support column, the other end and the B rotary device's of arm bottom are connected, four rotor unmanned aerial vehicle passes through C rotary device and is connected with B rotary device, control system passes through wireless communication technology with the arm and is connected. The utility model discloses degree of automation is high, and the function is comprehensive, and four rotor unmanned aerial vehicle's the maintenance work such as flying, retrieving and using required charging after is automated control, labour saving and time saving reduces the cost of labor.
Description
Technical Field
The utility model relates to an automatic four rotor unmanned aerial vehicle receive and release system who changes belongs to unmanned air vehicle technical field.
Background
Nowadays, the use of quad-rotor unmanned aerial vehicles is more and more widespread, but the maintenance work such as the charge that needs of unmanned aerial vehicle after the release, recovery and use all needs to be accomplished by the manual work at present. This also leads to if want large-scale use unmanned aerial vehicle must pay out a large amount of manpowers on unmanned aerial vehicle receive and releases and the logistical maintenance, this has increaseed the cost of labor greatly for this kind of automation equipment's that should alleviate the manpower burden value greatly reduced of unmanned aerial vehicle, lead to this emerging technique of unmanned aerial vehicle to be difficult to provide service for masses in wider field.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an automatic four rotor unmanned aerial vehicle receive and release system, the utility model discloses degree of automation is high, and the function is comprehensive, and unmanned aerial vehicle's the maintenance work such as flying, retrieving and using required charging after is automated control, labour saving and time saving reduces the cost of labor.
In order to solve the technical problem, the utility model discloses a following technical scheme: the utility model provides an automatic four rotor unmanned aerial vehicle receive and release system of changing, including the hangar, the support column, the arm, four rotor unmanned aerial vehicle, a control system, A rotary device, B rotary device and C rotary device, the support column sets up at the hangar middle part, the outer wall of support column is D1 with the distance of hangar, the one end of arm is passed through A rotary device and is connected with the support column, the other end and the B rotary device's of arm are connected, four rotor unmanned aerial vehicle passes through C rotary device and is connected with B rotary device, control system passes through wireless communication technology with the arm and is connected, degree of automation is high, the function is comprehensive, four rotor unmanned aerial vehicle's the flying, the required maintenance work such as charging is automated control after retrieving and using, time saving and labor saving, and labor cost is reduced.
According to the automatic four-rotor unmanned aerial vehicle retraction system, the hangar is of a circular ring structure, the supporting columns are arranged at the circle center position of the hangar, the hangar comprises a plurality of compartments, the compartments are internally provided with the charging modules and the electric quantity monitoring modules, and the charging modules are connected with the electric quantity monitoring modules through lines; four rotor unmanned aerial vehicle retrieve to the compartment after, electric quantity monitoring module monitors four rotor unmanned aerial vehicle's electric quantity, and when the electric quantity was not enough, electric quantity monitoring module sent the instruction of charging to the module of charging, and the module of charging charges four rotor unmanned aerial vehicle, and the electric quantity is full of the back, and electric quantity monitoring module sends the outage instruction to the module of charging, and the module of charging stops to charge four rotor unmanned aerial vehicle, and electric quantity monitoring module has avoided the phenomenon of overcharging.
According to the automatic four-rotor unmanned aerial vehicle retraction system, four groups of slideways are arranged on the supporting column at equal intervals on the circumference, the rotating device A is connected with the slideways in a sliding manner, the bottom of the supporting column is provided with a supporting base, and the supporting base is arranged at the circle center position of the hangar; the slide makes A rotary device can realize that the robotic arm is put away to four rotor unmanned aerial vehicle and is flown, retrieve the operation along the reciprocating up-and-down motion of support column circulation.
According to the automatic four-rotor unmanned aerial vehicle retraction system, an external module is arranged at the bottom of the four-rotor unmanned aerial vehicle and is in line connection with the four-rotor unmanned aerial vehicle, the external module comprises a shell and an external bottom plate, and the external bottom plate is connected with the bottom of the four-rotor unmanned aerial vehicle through the shell; the external module realizes the online control of the quad-rotor unmanned aerial vehicle.
According to the automatic four-rotor unmanned aerial vehicle retraction system, the charging module comprises a power supply box, a magnet A and a power supply device A are arranged on the power supply box, the magnet A is arranged above the power supply device A, a spring A is arranged at the bottom of the power supply box, and the bottom of the power supply box is connected with the bottom surface of the compartment through the spring A; when electric quantity monitoring module sent the instruction of charging to the module of charging, A magnet adsorbs four rotor unmanned aerial vehicle, and A power supply unit charges the operation to four rotor unmanned aerial vehicle, and when electric quantity monitoring module sent the outage instruction to the module of charging, A magnet stopped adsorbing four rotor unmanned aerial vehicle, and A power supply unit stopped charging four rotor unmanned aerial vehicle.
The automatic four-rotor unmanned aerial vehicle retraction system comprises a shell, a power supply device and a charging interface, wherein one end of the spring B is connected with the shell, one end of the spring B is connected with the electromagnet A, the electromagnet A is connected with the power supply device B, two ends of the power supply device B are connected with the shell, and the power supply device B is arranged above the charging interface; when electric quantity monitoring module sent the charging instruction to the module that charges, A magnet adsorbs the A electro-magnet, and A power supply unit charges four rotor unmanned aerial vehicle with the interface intercommunication that charges, and when electric quantity monitoring module sent the outage instruction to the module that charges, A magnet stopped adsorbing the A electro-magnet, A power supply unit with charge interface disconnection.
The utility model provides an automatic four rotor unmanned aerial vehicle receive and release system of changing, external bottom plate middle part is provided with the round hole that runs through, supreme C spring, B electro-magnet and the C power supply unit of having set gradually is down followed to the upper surface of external bottom plate, the lower surface of external bottom plate has set gradually the depressed part from inside to outside, copper ring and copper sheet, the diameter of C spring is greater than the diameter of round hole, the section of B electro-magnet is T style of calligraphy structure, the top diameter of B electro-magnet is greater than the diameter of C spring, the bottom diameter of B electro-magnet is less than the diameter of round hole, the round hole is worn to locate by the bottom of B electro-magnet, the depressed part diameter is greater than the diameter of B electro-magnet.
According to the automatic four-rotor unmanned aerial vehicle retraction system, the bottom of the rotating device C is connected with the top of the rotating device B, the rotating device C comprises a protruding column, a rotating part and an outer ring which are sequentially arranged from inside to outside, the protruding column is fixedly connected with the rotating part, the rotating part is movably connected with the outer ring, a metal probe is arranged on the rotating part, a metal connecting sheet is arranged on the outer ring, the inner diameter of the concave part is the same as the outer diameter of the protruding column, the depth of the concave part is the same as the height of the protruding column protruding out of the rotating part, and the protruding column is an electromagnet column; when retrieving four rotor unmanned aerial vehicle, protruding post is connected with the depressed part, and metal probe is connected with the copper ring, makes C rotary device and external module electricity intercommunication, and protruding post adsorbs with the B electro-magnet, makes B electro-magnet and C power supply unit disconnection, and four rotor unmanned aerial vehicle stop motion, the rotating part rotates, makes metal splicing and copper sheet contact, and the rotating part stall.
The control system comprises a positioning module, a mechanical arm control module and a compartment control module; the positioning module controls the motion direction of the mechanical arm, the positioning module adopts an ultra wide band wireless communication positioning technology, and after positioning information of the quad-rotor unmanned aerial vehicle is received, the mechanical arm can be accurately butted with the quad-rotor unmanned aerial vehicle, so that the quad-rotor unmanned aerial vehicle can be accurately released and recovered; compartment control module monitors the in service behavior of compartment, and compartment control module and arm control module cooperate, realize carrying out automated control to four rotor unmanned aerial vehicle's storage.
In the automatic four-rotor unmanned aerial vehicle retraction system, the rotating device A, the rotating device B and the rotating device C are all steering engines; a rotary device is a 360-degree controllable angle steering engine, B rotary device is a 180-degree controllable angle steering engine, and C rotary device is a 360-degree continuous rotation steering engine, and can meet the use requirements of mechanical arms and quad-rotor unmanned aerial vehicles.
Compared with the prior art, the utility model comprises a hangar, a support column, an mechanical arm, a quadrotor unmanned aerial vehicle, a control system, a rotating device A, a rotating device B and a rotating device C, wherein the control system is connected with the mechanical arm through a wireless communication technology, the control system is connected with the quadrotor unmanned aerial vehicle through a wireless communication technology, the hangar comprises a plurality of compartments, and charging modules, electric quantity monitoring modules and partition plates are arranged in the compartments, after the quadrotor unmanned aerial vehicle is recovered to the compartments, the electric quantity monitoring modules monitor the electric quantity of the quadrotor unmanned aerial vehicle, when the electric quantity is insufficient, the electric quantity monitoring modules send charging instructions to the charging modules, the charging modules charge the quadrotor unmanned aerial vehicle, after the electric quantity is full, the electric quantity monitoring modules send power-off instructions to the charging modules, the charging modules stop charging the quadrotor unmanned aerial vehicle, and the electric quantity monitoring modules avoid the phenomenon of overcharging, control system includes orientation module, unmanned aerial vehicle control module, arm control module and compartment control module, and the multimode is mutually supported, realizes flying, retrieving, storing and charging four rotor unmanned aerial vehicle and carries out automated control, the utility model discloses degree of automation is high, and the function is comprehensive, and four rotor unmanned aerial vehicle fly, retrieve and use required storage and the maintenance work such as charging after be automated control, labour saving and time saving reduce the cost of labor.
Drawings
Fig. 1 is a schematic structural diagram of the present invention;
FIG. 2 is a schematic view of the structure of the middle compartment of the present invention;
fig. 3 is a schematic structural diagram of a charging module and a housing in the present invention;
FIG. 4 is a schematic structural view of the middle hangar, the supporting columns and the supporting base of the present invention;
fig. 5 is a schematic structural view of a middle support column, an a-rotation device, a mechanical arm and a quad-rotor unmanned aerial vehicle according to the present invention;
FIG. 6 is a schematic structural view of the middle and outer hanging bottom plates and the C power supply device of the present invention;
FIG. 7 is a cross-sectional view of the plug-in module of the present invention;
fig. 8 is a schematic structural view of a C rotating device according to the present invention;
fig. 9 is a schematic diagram of the control system of the present invention.
Reference numerals: 1-hangar, 2-support column, 3-mechanical arm, 4-four-rotor unmanned aerial vehicle, 5-control system, 6-A rotating device, 7-B rotating device, 8-C rotating device, 9-compartment, 10-charging module, 11-electric quantity monitoring module, 12-slideway, 13-support base, 14-external module, 15-shell, 16-external bottom plate, 17-power box, 18-A magnet, 19-A power supply device, 20-A spring, 21-B spring, 22-A electromagnet, 23-B power supply device, 24-charging interface, 25-round hole, 26-C spring, 27-B electromagnet, 28-C power supply device, 29-recess and 30-copper ring, 31-copper sheet, 32-convex column, 33-rotary part, 34-outer ring, 35-metal probe, 36-metal contact.
The present invention will be further described with reference to the accompanying drawings and the detailed description.
Detailed Description
Embodiment 5 of the utility model: the utility model provides an automatic four rotor unmanned aerial vehicle receive and release system, including hangar 1, support column 2, arm 3, four rotor unmanned aerial vehicle 4, control system 5, A rotary device 6, B rotary device 7 and C rotary device 8, support column 2 sets up in hangar 1 middle part, the outer wall of support column 2 is D1 with hangar 1's distance, arm 3's one end is connected with support column 2 through A rotary device 6, arm 3's the other end is connected with B rotary device 7's bottom, four rotor unmanned aerial vehicle 4 is connected with B rotary device 7 through C rotary device 8, control system 5 is connected through wireless communication technique with arm 3, degree of automation is high, the function is comprehensive, four rotor unmanned aerial vehicle 4's the maintenance work such as releasing, required charging after retrieving and using is automatic control, time saving and labor saving, labor cost is reduced; the hangar 1 is of a circular ring structure, the supporting columns 2 are arranged at the circle center of the hangar 1, the hangar 1 comprises a plurality of compartments 9, charging modules 10 and electric quantity monitoring modules 11 are arranged in the compartments 9, and the charging modules 10 are connected with the electric quantity monitoring modules 11 through lines; after the quad-rotor unmanned aerial vehicle 4 is recovered to the compartment 9, the electric quantity monitoring module 11 monitors the electric quantity of the quad-rotor unmanned aerial vehicle 4, when the electric quantity is insufficient, the electric quantity monitoring module 11 sends a charging instruction to the charging module 10, the charging module 10 charges the quad-rotor unmanned aerial vehicle 4, after the electric quantity is full, the electric quantity monitoring module 11 sends a power-off instruction to the charging module 10, the charging module 10 stops charging the quad-rotor unmanned aerial vehicle 4, and the electric quantity monitoring module 11 avoids an overcharging phenomenon; four groups of slideways 12 are circumferentially arranged on the supporting column 2 at equal intervals, the rotating device A6 is connected with the slideways 12 in a sliding manner, a supporting base 13 is arranged at the bottom of the supporting column 2, and the supporting base 13 is arranged at the position of the circle center of the hangar 1; the slide way 12 enables the rotating device A6 to move up and down along the support column 2 in a reciprocating mode, and the release and recovery operations of the mechanical arm 3 on the quad-rotor unmanned aerial vehicle 4 are achieved; the bottom of the quad-rotor unmanned aerial vehicle 4 is provided with an external module 14, the external module 14 is in line connection with the quad-rotor unmanned aerial vehicle 4, the external module 14 comprises a shell 15 and an external bottom plate 16, and the external bottom plate 16 is connected with the bottom of the quad-rotor unmanned aerial vehicle 4 through the shell 15; the external hanging module 14 realizes the positioning and capturing of the four-rotor unmanned aerial vehicle 4 by the mechanical arm 3; the charging module 10 comprises a power supply box 17, wherein an A magnet 18 and an A power supply device 19 are arranged on the power supply box 17, the A magnet 18 is arranged above the A power supply device 19, an A spring 20 is arranged at the bottom of the power supply box 17, and the bottom of the power supply box 17 is connected with the bottom surface of the compartment 9 through the A spring 20; when electric quantity monitoring module 11 sends the instruction of charging to charging module 10, A magnet 18 adsorbs four rotor unmanned aerial vehicle 4, and A power supply unit 19 charges operation to four rotor unmanned aerial vehicle 4, and when electric quantity monitoring module 11 sends the outage instruction to charging module 10, A magnet 18 stops adsorbing four rotor unmanned aerial vehicle 4, and A power supply unit 19 stops charging to four rotor unmanned aerial vehicle 4.
The utility model discloses a theory of operation of embodiment: when the utility model is used for recovering the quadrotor unmanned aerial vehicle 4, the mechanical arm 3 is extended, the positioning module mechanical arm 3 sends out positioning data, the A rotating device 6 drives the mechanical arm 3 to rotate to an accurate position according to the positioning data, the C rotating device 8 is butted with the external hanging module 14, the convex column 32 is connected with the concave part 29, the metal probe 35 is connected with the copper ring 30, the C rotating device 8 is electrically communicated with the external hanging module 14, the convex column 32 is adsorbed by the B electromagnet 27, the B electromagnet 27 is disconnected with the C power supply device 28, the quadrotor unmanned aerial vehicle 4 stops moving, the rotating part 33 rotates, the metal splicing sheet 36 is contacted with the copper sheet 31, the mechanical arm 3 is retracted, the A rotating device 6 drives the mechanical arm 3 to move downwards along the supporting column 2, the compartment control module sends out unused data of the compartment 9, the mechanical arm 3 recovers the quadrotor unmanned aerial vehicle 4 to the unused compartment 9 according to the unused data of the compartment 9, the compartment control module records use information of the compartment 9, the A magnet 18 adsorbs the A electromagnet 22, the A power supply device 19 is communicated with the charging interface 24, the electric quantity monitoring module 11 monitors the electric quantity of the quad-rotor unmanned aerial vehicle 4, when the electric quantity is insufficient, the A magnet charges the quad-rotor unmanned aerial vehicle 4 when the electric quantity monitoring module 11 sends a charging instruction to the charging module 10, and when the electric quantity monitoring module 11 sends a power-off instruction to the charging module 10, the A power supply device 19 stops supplying power to the A magnet; when the quad-rotor unmanned aerial vehicle 4 is released, the positioning module is matched with the compartment control module to determine the quad-rotor unmanned aerial vehicle 4 to be released, then the mechanical arm 3 is sent out positioning data, the A rotating device 6 drives the mechanical arm 3 to rotate to the accurate compartment 9 according to the positioning data, the mechanical arm 3 is extended, the C rotating device 8 is butted with the external hanging module 14, the convex column 32 is connected with the concave part 29, the metal probe 35 is connected with the copper ring 30, the C rotating device 8 is electrically communicated with the external hanging module 14, the convex column 32 is adsorbed with the B electromagnet 27, the quad-rotor unmanned aerial vehicle 4 to be released is taken out, the mechanical arm 3 is retracted, the A rotating device 6 drives the mechanical arm 3 to move upwards along the supporting column 2, the compartment control module records the use information of the compartment 9, the mechanical arm 3 is extended again, the rotating part 33 rotates, the metal splicing 36 is disconnected with the copper sheet 31, the convex column 32 is separated from the B electromagnet 27 for adsorption, the B electromagnet 27 is connected to the C power supply device 28, and the quad-rotor drone 4 starts to move.
Claims (10)
1. The utility model provides an automatic four rotor unmanned aerial vehicle receive and release system of changing, a serial communication port, including hangar (1), support column (2), arm (3), four rotor unmanned aerial vehicle (4), control system (5), A rotary device (6), B rotary device (7) and C rotary device (8), support column (2) set up at hangar (1) middle part, the outer wall of support column (2) is D1 with the distance of hangar (1), the one end of arm (3) is passed through A rotary device (6) and is connected with support column (2), the other end and the bottom of B rotary device (7) of arm (3) are connected, four rotor unmanned aerial vehicle (4) are connected with B rotary device (7) through C rotary device (8), control system (5) are connected through wireless communication technology with arm (3).
2. The automatic four rotor unmanned aerial vehicle receive and releases system of claim 1, characterized in that, hangar (1) is the ring structure, and support column (2) are arranged in the centre of a circle position of hangar (1), and hangar (1) includes a plurality of compartments (9), be provided with in compartment (9) charging module (10) and electric quantity monitoring module (11), charging module (10) and electric quantity monitoring module (11) line connection.
3. An automated four-rotor unmanned aerial vehicle retraction system according to claim 1, wherein four sets of slides (12) are circumferentially arranged on the support column (2) at equal intervals, the rotating device A (6) is slidably connected with the slides (12), a support base (13) is arranged at the bottom of the support column (2), and the support base (13) is arranged at the position of the center of a circle of the hangar (1).
4. The automatic four-rotor unmanned aerial vehicle retraction system according to claim 1, wherein an external hanging module (14) is arranged at the bottom of the four-rotor unmanned aerial vehicle (4), the external hanging module (14) is in line connection with the four-rotor unmanned aerial vehicle (4), the external hanging module (14) comprises a shell (15) and an external hanging bottom plate (16), and the external hanging bottom plate (16) is connected with the bottom of the four-rotor unmanned aerial vehicle (4) through the shell (15).
5. An automated four-rotor unmanned aerial vehicle retraction system according to claim 2, wherein the charging module (10) comprises a power supply box (17), an A magnet (18) and an A power supply device (19) are arranged on the power supply box (17), the A magnet (18) is arranged above the A power supply device (19), an A spring (20) is arranged at the bottom of the power supply box (17), and the bottom of the power supply box (17) is connected with the bottom surface of the compartment (9) through the A spring (20).
6. The automatic four-rotor unmanned aerial vehicle retraction system according to claim 4, wherein the housing (15) comprises a B spring (21), an A electromagnet (22), a B power supply device (23) and a charging interface (24), one end of the B spring (21) is connected with the housing (15), one end of the B spring (21) is connected with the A electromagnet (22), the A electromagnet (22) is connected with the B power supply device (23), two ends of the B power supply device (23) are connected with the housing (15), and the B power supply device (23) is arranged above the charging interface (24).
7. The automatic four-rotor unmanned aerial vehicle retraction system according to claim 4, wherein a through circular hole (25) is formed in the middle of the external base plate (16), a C spring (26), a B electromagnet (27) and a C power supply device (28) are sequentially arranged on the upper surface of the external base plate (16) from bottom to top, a recessed portion (29), a copper ring (30) and a copper sheet (31) are sequentially arranged on the lower surface of the external base plate (16) from inside to outside, the circular hole (25) is formed in the middle of the recessed portion (29), the diameter of the C spring (26) is larger than that of the circular hole (25), the section of the B electromagnet (27) is of a T-shaped structure, the diameter of the top of the B electromagnet (27) is larger than that of the C spring (26), the diameter of the bottom of the B electromagnet (27) is smaller than that of the circular hole (25), the bottom of the B electromagnet (27) penetrates through the circular hole (25), the diameter of the concave part (29) is larger than that of the B electromagnet (27).
8. The automatic four rotor unmanned aerial vehicle receive and release system of claim 7, characterized in that, the bottom of C rotary device (8) is connected with the top of B rotary device (7), C rotary device (8) is including protruding post (32), rotating part (33) and outer loop (34) that arrange from inside to outside in proper order, protruding post (32) and rotating part (33) fixed connection, rotating part (33) and outer loop (34) swing joint, be provided with metal probe (35) on rotating part (33), be provided with metal splicing (36) on outer loop (34), the internal diameter of depressed part (29) is the same with the external diameter of protruding post (32), the degree of depth of depressed part (29) is the same with the height that protruding post (32) magnet protrusion in rotating part (33), protruding post (32) are the electricity post.
9. An automated quad-rotor drone deploying and retracting system according to claim 1, characterized in that the control system (5) comprises a positioning module, a mechanical arm control module and a compartment control module.
10. An automated quad-rotor drone deploying and retracting system according to claim 1, wherein the rotating device a (6), the rotating device B (7) and the rotating device C (8) are all steering engines.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120366078.0U CN214986136U (en) | 2021-02-09 | 2021-02-09 | Automatic four rotor unmanned aerial vehicle who changes receive and release system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120366078.0U CN214986136U (en) | 2021-02-09 | 2021-02-09 | Automatic four rotor unmanned aerial vehicle who changes receive and release system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214986136U true CN214986136U (en) | 2021-12-03 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120366078.0U Expired - Fee Related CN214986136U (en) | 2021-02-09 | 2021-02-09 | Automatic four rotor unmanned aerial vehicle who changes receive and release system |
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| CN (1) | CN214986136U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2024016807A1 (en) * | 2022-07-19 | 2024-01-25 | 比亚迪股份有限公司 | Unmanned aerial vehicle rack, hangar and vehicle |
-
2021
- 2021-02-09 CN CN202120366078.0U patent/CN214986136U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2024016807A1 (en) * | 2022-07-19 | 2024-01-25 | 比亚迪股份有限公司 | Unmanned aerial vehicle rack, hangar and vehicle |
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| CF01 | Termination of patent right due to non-payment of annual fee | ||
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Granted publication date: 20211203 |