CN112722256A - Formation performance unmanned aerial vehicle system - Google Patents
Formation performance unmanned aerial vehicle system Download PDFInfo
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- CN112722256A CN112722256A CN202110053553.3A CN202110053553A CN112722256A CN 112722256 A CN112722256 A CN 112722256A CN 202110053553 A CN202110053553 A CN 202110053553A CN 112722256 A CN112722256 A CN 112722256A
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- unmanned aerial
- aerial vehicle
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- formation performance
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- 230000015572 biosynthetic process Effects 0.000 title claims abstract description 18
- 230000005540 biological transmission Effects 0.000 claims description 13
- 238000004891 communication Methods 0.000 claims description 13
- 238000013500 data storage Methods 0.000 claims description 10
- 230000001681 protective effect Effects 0.000 claims description 5
- 230000002457 bidirectional effect Effects 0.000 claims description 3
- 238000000034 method Methods 0.000 abstract description 5
- 238000010586 diagram Methods 0.000 description 2
- 206010016322 Feeling abnormal Diseases 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
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- 238000006467 substitution reaction Methods 0.000 description 1
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
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Abstract
The invention relates to the technical field of unmanned aerial vehicles, and discloses a formation performance unmanned aerial vehicle system, which comprises an unmanned aerial vehicle, a control system, an LED light-emitting plate is embedded in the top center of the unmanned aerial vehicle, fixing plates are fixedly connected to the upper end and the lower end of the left side and the right side of an unmanned main body, a connecting plate is connected to the tail end of each fixing plate in a rotating mode, a rotating motor is fixedly arranged at the tail end of each connecting plate, a spiral blade is installed at the output end of each rotating motor, the system drives the spiral blade to drive the unmanned aerial vehicle to take off through the rotating motor, the distance and the angle of the spiral blade are controlled through the rotation of the connecting plates in the fixing plates, the flying state of the unmanned aerial vehicle is adjusted, the stability of the unmanned aerial vehicle in the flying process is improved, accurate indoor positioning data, Temperature, etc.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to a formation performance unmanned aerial vehicle system.
Background
The unmanned aerial vehicle is provided with no cockpit, but is provided with an automatic pilot, a program control device and other equipment. Ground, on the naval vessel or mother's aircraft remote control station personnel pass through equipment such as radar, track it, location, remote control, telemetering measurement and digital transmission, and along with the development unmanned aerial vehicle of scientific and technological walk people's daily life gradually, unmanned aerial vehicle cluster performance often appears in large-scale commercial tandem, for getting the smoothness of guarantor unmanned aerial vehicle formation performance, needs control system to control unmanned aerial vehicle.
At present, current unmanned aerial vehicle controls through remote control handle more, and control distance is limited, can't obtain unmanned aerial vehicle's positional information, image video, battery power information are accurate, and unmanned aerial vehicle's flight process is stable not good.
Disclosure of Invention
Aiming at the defects of the prior art, the invention provides a formation performance unmanned aerial vehicle system, which solves the problems that the existing unmanned aerial vehicle is controlled by a remote control handle, the control distance is limited, the position information, the image video and the battery power information of the unmanned aerial vehicle cannot be accurately acquired, and the stability of the unmanned aerial vehicle in the flying process is poor.
The invention provides the following technical scheme: the utility model provides a formation performance unmanned aerial vehicle system, includes unmanned aerial vehicle, control system, unmanned aerial vehicle's top center is embedded to have the LED luminescent plate, fixedly connected with fixed plate about the left and right sides of unmanned house main part, the end-to-end rotation of fixed plate is connected with the connecting plate, the end-to-end fixation of connecting plate is provided with the rotation motor, helical blade is installed to the output of rotating the motor, unmanned aerial vehicle's bottom left and right sides is rotated and is installed the undercarriage, the bottom fixedly connected with blotter of undercarriage, unmanned aerial vehicle's the fixed battery that is provided with in the middle of the inside, fixed mounting has the pivot in the middle of unmanned aerial vehicle's the bottom, protecting sheathing is installed to.
Preferably: the control system is composed of a GPS module, a camera module, a power supply module, a data storage module, a main control module, a communication module, a server and a mobile phone terminal APP.
Preferably: the cushion pad is made of a material with high elasticity and softness.
Preferably: the storage battery is electrically connected with the rotating motor, the LED light-emitting plate and the camera through wires.
Preferably: the GPS module, the camera module, the power supply module, the data storage module, the main control module and the communication module are arranged inside the unmanned aerial vehicle.
Preferably: the upper end of the undercarriage is arc-shaped and is bent outwards, and the lower end of the undercarriage is vertical.
Preferably: data transmission among the GPS module, the camera module, the power supply module and the data storage module is unidirectional transmission, and data transmission between the main control module and the communication module, between the communication module and the server, between the server and the mobile phone terminal APP is bidirectional transmission.
Preferably: the tail end of the landing gear is lower than the bottom of the protective shell.
Compared with the prior art, the invention has the following beneficial effects:
1. the utility model provides a formation performance unmanned aerial vehicle system, drives unmanned aerial vehicle through rotating motor drive helical blade and takes off, and four helical blade of group promote unmanned aerial vehicle flight power, through the distance and the angle of the rotation control helical blade of connecting plate in the fixed plate, and then adjust unmanned aerial vehicle flight state, promote the stability of unmanned aerial vehicle flight in-process.
2. The utility model provides a formation performance unmanned aerial vehicle system, provides the accurate indoor location data of unmanned aerial vehicle through the GPS module, provides image, the video information that unmanned aerial vehicle shot through the camera module, provides information such as battery power, temperature in the unmanned aerial vehicle through power module.
Drawings
Fig. 1 is a schematic diagram of the overall overhead structure of the unmanned aerial vehicle of the present invention;
FIG. 2 is a schematic view of a front view of the unmanned aerial vehicle of the present invention;
FIG. 3 is a block diagram of the system control of the unmanned aerial vehicle of the present invention;
in the figure: 1. an unmanned aerial vehicle; 2. an LED light emitting panel; 3. a rotation motor; 4. a helical blade; 5. a connecting plate; 6. a fixing plate; 7. a landing gear; 8. a rotating shaft; 9. a camera; 10. a cushion pad; 11. a rotating shaft; 12. a storage battery; 13. and (5) controlling the system.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-3, a formation performance unmanned aerial vehicle system comprises an unmanned aerial vehicle 1, a control system 13, an LED light-emitting panel 2 embedded in the top center of the unmanned aerial vehicle 1, fixing plates 6 fixedly connected to the upper and lower sides of the left and right sides of the unmanned main body 1, a connecting plate 5 rotatably connected to the end of the fixing plate 6, a rotating motor 3 fixedly disposed at the end of the connecting plate 5, a helical blade 4 mounted at the output end of the rotating motor 3, landing gears 7 rotatably mounted at the left and right sides of the bottom of the unmanned aerial vehicle 1, a cushion pad 10 fixedly connected to the bottom of the landing gears 7, the cushion pad 10 made of a high-elasticity and soft-feeling material, a storage battery 12 fixedly disposed in the middle of the interior of the unmanned aerial vehicle 1, a rotating shaft 11 fixedly mounted in the middle of the bottom of the unmanned aerial vehicle, and undercarriage 7's end is less than 8 bottoms of protecting sheathing, protecting sheathing 8's center is rotated and is installed camera 9, battery 12 and rotation motor 3, LED luminescent plate 2, camera 9 passes through wire electric connection, control system 13 is by the GPS module, camera module, power module, data storage module, host system, communication module, a server, cell-phone terminal APP constitutes jointly, the GPS module, camera module, power module, data storage module, host system, communication module sets up inside unmanned aerial vehicle, the GPS module, camera module, data transmission is unidirectional transmission between power module and the data storage module, host system and communication module, communication module and server, server and cell-phone terminal APP data transmission are bidirectional transmission.
During working, a plurality of unmanned aerial vehicles 1 are stably placed by workers to form an unmanned aerial vehicle cluster, the unmanned aerial vehicles 1 emit light at night through the LED light-emitting plates 2, so that a user can conveniently observe, use and track at night, and the rotating motor 3 drives the helical blades 4 to drive the unmanned aerial vehicles 1 to take off;
the four groups of helical blades 4 improve the flight power of the unmanned aerial vehicle 1, the distance and the angle of the helical blades 4 are controlled through the rotation of the connecting plate 5 in the fixing plate 6, the flight state of the unmanned aerial vehicle 1 is further adjusted, and the stability of the unmanned aerial vehicle 1 in the flight process is improved;
secondly, the camera 9 is protected through the protective shell 8, the angle of the camera 9 is adjusted through the rotating shaft 11, the shooting range of the camera 9 is enlarged, impact force and vibration generated when the unmanned aerial vehicle 1 lands are reduced through the undercarriage 7 and the cushion pad 10, the unmanned aerial vehicle 1 lands more stably, and then electric energy is provided for the rotating motor 3, the LED light-emitting panel 2 and the camera 9 through the storage battery 12;
finally, the GPS module provides accurate indoor positioning data of the unmanned aerial vehicle 1, the camera module provides images and video information shot by the unmanned aerial vehicle 1, the power supply module provides information such as the electric quantity and the temperature of a storage battery in the unmanned aerial vehicle 1, the information is stored by the data storage module and then enters the main control module, and the main control module uploads the data to the server through the communication module;
carry out data and look over through cell-phone terminal APP to this user can be on cell-phone terminal APP accurate acquire arbitrary unmanned aerial vehicle 1's in the unmanned aerial vehicle cluster positional information, image video, battery power state and unmanned aerial vehicle 1 flight state, can control and operate unmanned aerial vehicle 1 information through cell-phone terminal APP simultaneously, can issue and receive unmanned aerial vehicle 1 flight performance, and rent or purchase unmanned aerial vehicle 1 product.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (8)
1. A formation performance drone system, comprising a drone (1), a control system (13), characterized in that: an LED light-emitting plate (2) is embedded in the center of the top of the unmanned aerial vehicle (1), fixing plates (6) are fixedly connected to the upper end and the lower end of the left side and the right side of the unmanned aerial vehicle main body (1), the tail end of the fixed plate (6) is rotationally connected with a connecting plate (5), the tail end of the connecting plate (5) is fixedly provided with a rotating motor (3), the output end of the rotating motor (3) is provided with a helical blade (4), the left side and the right side of the bottom of the unmanned aerial vehicle (1) are provided with undercarriage (7) in a rotating way, the bottom of the landing gear (7) is fixedly connected with a cushion pad (10), the middle inside the unmanned aerial vehicle (1) is fixedly provided with a storage battery (12), a rotating shaft (11) is fixedly installed in the middle of the bottom of the unmanned aerial vehicle (1), a protective shell (8) is installed at the bottom of the rotating shaft (11), the center of the protective shell (8) is rotatably provided with a camera (9).
2. A formation performance drone system according to claim 1, wherein: the control system (13) is composed of a GPS module, a camera module, a power supply module, a data storage module, a main control module, a communication module, a server and a mobile phone terminal APP.
3. A formation performance drone system according to claim 1, wherein: the cushion pad (10) is made of a material having high elasticity and softness.
4. A formation performance drone system according to claim 1, wherein: the storage battery (12) is electrically connected with the rotating motor (3), the LED light-emitting plate (2) and the camera (9) through wires.
5. A formation performance drone system according to claim 2, wherein: the GPS module, the camera module, the power supply module, the data storage module, the main control module and the communication module are arranged inside the unmanned aerial vehicle.
6. A formation performance drone system according to claim 1, wherein: the upper end of the landing gear (7) is arc-shaped and is bent outwards, and the lower end of the landing gear is vertical.
7. A formation performance drone system according to claim 2, wherein: data transmission among the GPS module, the camera module, the power supply module and the data storage module is unidirectional transmission, and data transmission between the main control module and the communication module, between the communication module and the server, between the server and the mobile phone terminal APP is bidirectional transmission.
8. A formation performance drone system according to claim 1, wherein: the tail end of the landing gear (7) is lower than the bottom of the protective shell (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110053553.3A CN112722256A (en) | 2021-01-15 | 2021-01-15 | Formation performance unmanned aerial vehicle system |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110053553.3A CN112722256A (en) | 2021-01-15 | 2021-01-15 | Formation performance unmanned aerial vehicle system |
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| CN112722256A true CN112722256A (en) | 2021-04-30 |
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| CN202110053553.3A Pending CN112722256A (en) | 2021-01-15 | 2021-01-15 | Formation performance unmanned aerial vehicle system |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114020029A (en) * | 2021-11-09 | 2022-02-08 | 深圳大漠大智控技术有限公司 | Automatic generation method and device of aerial route for cluster and related components |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20170092205A (en) * | 2016-02-03 | 2017-08-11 | 한양대학교 에리카산학협력단 | Flight Control Method of Unmanned Aerial Vehicle Based on Ultra Wideband Location and Apparatus therefor, Ultra Wideband Based Location System |
| CN207072428U (en) * | 2017-08-08 | 2018-03-06 | 厦门神龙航空科技有限公司 | Unmanned plane with adjustable-angle horn |
| CN207516832U (en) * | 2017-06-21 | 2018-06-19 | 深圳大漠大智控技术有限公司 | The landing control system of taking off of unmanned plane formation performance |
| CN207985184U (en) * | 2018-03-13 | 2018-10-19 | 清远市巨劲科技有限公司 | A kind of collapsible unmanned plane of taking photo by plane |
| US20190052865A1 (en) * | 2017-12-28 | 2019-02-14 | Intel IP Corporation | Dynamic baseline depth imaging using multiple drones |
| US20190391575A1 (en) * | 2017-04-28 | 2019-12-26 | Ars Electronica Linz Gmbh & Co Kg | Unmanned aircraft with a modular swarm control unit |
| CN112027084A (en) * | 2020-09-10 | 2020-12-04 | 杭州企飞飞科技有限公司 | Civil unmanned aerial vehicle for photography recording |
-
2021
- 2021-01-15 CN CN202110053553.3A patent/CN112722256A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20170092205A (en) * | 2016-02-03 | 2017-08-11 | 한양대학교 에리카산학협력단 | Flight Control Method of Unmanned Aerial Vehicle Based on Ultra Wideband Location and Apparatus therefor, Ultra Wideband Based Location System |
| US20190391575A1 (en) * | 2017-04-28 | 2019-12-26 | Ars Electronica Linz Gmbh & Co Kg | Unmanned aircraft with a modular swarm control unit |
| CN207516832U (en) * | 2017-06-21 | 2018-06-19 | 深圳大漠大智控技术有限公司 | The landing control system of taking off of unmanned plane formation performance |
| CN207072428U (en) * | 2017-08-08 | 2018-03-06 | 厦门神龙航空科技有限公司 | Unmanned plane with adjustable-angle horn |
| US20190052865A1 (en) * | 2017-12-28 | 2019-02-14 | Intel IP Corporation | Dynamic baseline depth imaging using multiple drones |
| CN207985184U (en) * | 2018-03-13 | 2018-10-19 | 清远市巨劲科技有限公司 | A kind of collapsible unmanned plane of taking photo by plane |
| CN112027084A (en) * | 2020-09-10 | 2020-12-04 | 杭州企飞飞科技有限公司 | Civil unmanned aerial vehicle for photography recording |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114020029A (en) * | 2021-11-09 | 2022-02-08 | 深圳大漠大智控技术有限公司 | Automatic generation method and device of aerial route for cluster and related components |
| CN114020029B (en) * | 2021-11-09 | 2022-06-10 | 深圳大漠大智控技术有限公司 | Automatic generation method and device of aerial route for cluster and related components |
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