CN210000581U - physical combined unmanned aerial vehicle cluster - Google Patents
physical combined unmanned aerial vehicle cluster Download PDFInfo
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- CN210000581U CN210000581U CN201822053723.4U CN201822053723U CN210000581U CN 210000581 U CN210000581 U CN 210000581U CN 201822053723 U CN201822053723 U CN 201822053723U CN 210000581 U CN210000581 U CN 210000581U
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Abstract
The utility model discloses an physics combination formula unmanned aerial vehicle cluster forms by many unmanned aerial vehicle units physics combination, the unmanned aerial vehicle unit includes hexagon head frame, casing, coaxial bispin wing, take off and land skid and modularization task unit, hexagon head frame passes through the support frame and fixes the casing at the frame center, take off and land skid is installed to the casing below, and coaxial bispin wing is connected at the casing top, modularization task unit sets up at chassis bottom, each limit of hexagon head frame all is equipped with interfacing apparatus, utilizes this interfacing apparatus to realize the physics combination of many unmanned aerial vehicle units, the utility model discloses an energy management and load distribution are realized to the direct physics network deployment of unmanned aerial vehicle, long and the task ability when having promoted the standby of whole cluster, have improved the task viability in the threat environment.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is kinds of physics combination formula unmanned aerial vehicle cluster.
Background
In the pearl ocean exhibition of 2016, China electronic science CETC discloses a th fixed wing unmanned aerial vehicle cluster test prototype system in China, 67-frame scale cluster principle verification is realized, world records of 50 fixed wing unmanned aerial vehicle clusters kept by the American navy before are broken through, and the cluster technology can be seen to be the lower hot spots of unmanned aerial vehicle technology development by combining with the subsequent aerial light shows of hundreds of multi-rotor unmanned aerial vehicle clusters emerging from various regions.
The unmanned aerial vehicle cluster is large in number, small-sized design is usually adopted for controlling cost, the structure is simple, and control is simple, however, small-sized unmanned aerial vehicles are short in endurance time and small in load, tasks which can be completed are reduced immediately, and the application prospect of the unmanned aerial vehicle cluster is greatly limited.
SUMMERY OF THE UTILITY MODEL
For solving the problem, the utility model provides an kinds of physics combination formula unmanned aerial vehicle cluster realizes energy management and load distribution through the direct physics network deployment of unmanned aerial vehicle, and length and task ability when promoting the standby of whole cluster.
kinds of physics combination formula unmanned aerial vehicle cluster forms by the physical combination of many unmanned aerial vehicle units, the unmanned aerial vehicle unit includes hexagon head frame, casing, coaxial bispin wing, take off and land skid and modularization task unit, hexagon head frame passes through the support frame and fixes the casing at the frame center, take off and land skid is installed to the casing below, and coaxial bispin wing is connected at the casing top, the setting of modularization task unit is at chassis bottom, each limit of hexagon head frame all is equipped with interfacing apparatus, utilizes this interfacing apparatus to realize the physical combination of many unmanned aerial vehicle units.
The telescopic solar thin film is arranged in the hexagonal head frame, and the solar power generation design with the telescopic solar thin film can draw and distribute energy sources on site, so that the cluster ultra-long task standby can be realized.
The side of hexagonal head frame is equipped with the fusion sensor/antenna for unmanned aerial vehicle data acquisition, receiving and dispatching.
The shell is internally provided with a power module, an energy storage module, a processing module, a communication module and other equipment. The power module is used for providing power for taking off, landing and flying of the unmanned aerial vehicle; the energy storage module is used for storing electric energy for the power module and also used for storing electric energy converted from light energy when the solar thin film is unfolded for power generation; the processing module is used for managing and controlling other modules; the communication module is used for data receiving, transmitting and transmitting.
The single unmanned aerial vehicle is driven by pure electricity and can take off, fly and land completely and autonomously.
Except that realizing unmanned aerial vehicle physical connection, still transmittable data and energy among the interfacing apparatus, jointly form the logic control brain of cluster with each unit processing module's operational capability based on distributed computing technology, can realize energy management behind the network deployment, for example what partial unmanned aerial vehicle unit in the network deployment carried is the reserve energy, offer other task unmanned aerial vehicles as the supply unit, still can close the driving system of some redundant unmanned aerial vehicle units in the network deployment, the solar energy film of expansion shrink at its hexagon head utilizes the real-time supply energy of solar energy, thereby the task standby during realization whole cluster long voyage.
The utility model has the advantages that:
1. the distributed cluster is adopted, resources required by high-value unmanned machines or large unmanned machines to complete tasks are dispersed into various small modularized task loads, the loads are carried by different unmanned machine single machines, and a large number of low-cost unmanned machine platforms are used for carrying out cooperative control among all the constituent units of the task components through the cluster to complete the tasks.
2. Due to the adoption of a modularized and generalized design, the method is low in manufacturing cost, can be configured aiming at task redundancy, improves the task completion rate, has small hit loss and incidental risk, and improves the task viability in a threatening environment.
3. The unmanned aerial vehicle can be in standby for the ultra-long task, a large-scale flying assembly, namely a combined unmanned aerial vehicle cluster, is formed by physically butting the single-unit networks of a plurality of unmanned aerial vehicles, the unmanned aerial vehicle cluster is combined with the self-contained solar power generation design of the unmanned aerial vehicle, energy is drawn on the spot and distributed, meanwhile, the power system of the unmanned aerial vehicle units with partial redundancy in the network is closed, a work cycle of 'executing task, returning to cluster butting, charging in real time, releasing again and executing task' is formed, and the standby for the ultra-.
Drawings
Fig. 1 is a front view of the unmanned aerial vehicle unit of the present invention;
FIG. 2 is a side view of FIG. 1;
FIG. 3 is a top view of FIG. 1;
FIG. 4 is a schematic view of the single side arrangement of the head frame of the present invention;
fig. 5 is a schematic diagram of the docking networking and separation of the physically combined unmanned aerial vehicle cluster of the present invention;
in the figure, 1, a take-off and landing skid, 2, a spherical shell, 3, a hexagonal head frame, 4, coaxial double rotors, 5, a fusion sensor/antenna, 6, a modular task unit, 7, a support frame, 8, a telescopic solar energy film, 9, a butt joint device, 10, a data and energy transmission channel, 11 and a laser positioning device.
Detailed Description
In order to deepen the understanding of the present invention, the present invention will be described in detail with reference to the following steps in combination with the embodiments and the drawings, the embodiments are only used for explaining the present invention, and do not constitute the limitation of the protection scope of the present invention.
As shown in fig. 1 to 4, an combined unmanned aerial vehicle cluster is a diamond-shaped cluster formed by physically combining 25 unmanned aerial vehicle units, wherein the selected unmanned aerial vehicle units (adopting pure electric drive and being capable of completely and autonomously taking off, flying and landing) have the following structures that a hexagonal head frame 3 (with closed sides, open top and bottom, top air intake and bottom air exhaust during flying), a spherical casing 2 (with light weight and convenient manufacture and good economic acceptance due to the adoption of a spherical shell design), coaxial double rotors 4, a take-off and landing skid 1 and a modular task unit 6 are adopted, the spherical casing 2 is fixed at the center of the frame by the hexagonal head frame 3 through three support frames 7 (with a module connected with the inside of the casing through a circuit inside the support frames), specifically, ends of the three support frames 7 are fixed with the spherical casing 2, and the other ends are fixed with three corners of the hexagonal head frame, and the included angles of the three support frames are 120 degrees.
The lifting skid 1 is installed below the spherical casing 2, the top of the spherical casing 2 is connected with the coaxial double rotors 4, single-machine vertical lifting and flying are achieved through the design of the lifting skid 1 and the coaxial double rotors 4, the requirements of the lifting skid on a lifting site are low, the task adaptability is strong, the coaxial double rotors 4 are used for providing lifting force and direction control of flying, the lifting force is provided and single propeller torque is balanced through rotation of the upper and lower double rotors which rotate around the same axis positive reverse, and the direction control can be achieved through the differential generation of unbalanced torque of the total distance of the upper and lower rotors.
The spherical shell 2 is internally provided with a power module, an energy storage module, a processing module, a communication module and other equipment, wherein the power module is used for providing power for taking off and landing and flying of the unmanned aerial vehicle, the energy storage module is used for storing electric energy for the power module and also used for storing electric energy converted from light energy when a solar thin film is unfolded for power generation, the processing module is used for managing and controlling other modules, the communication module is used for transmitting and receiving data, the modular task unit 6 is arranged at the bottom of the spherical shell 2, the modular task unit 6 comprises other functions such as reconnaissance, striking, communication and each independent unit to form task capacity, resources required by tasks are decomposed and miniaturized, the resources are carried by different unmanned aerial vehicle units, and the unmanned aerial vehicle units are in a large amount of low-cost consumable design, so that redundant configuration can be carried out to bring effect multiplication and improve task viability in a threat environment.
Be equipped with retractable solar energy film 8 in hexagonal head frame 3, this kind of design from taking solar power generation, when closing the driving system of part redundancy's unmanned aerial vehicle unit in the network deployment, the solar energy film of expansion shrink at its hexagonal head frame utilizes solar energy to supply on the spot in real time and draws the energy and distribute, has realized the super long task standby of whole cluster.
Each side of hexagon head frame 3 all is equipped with two interfacing apparatus 9 for unmanned aerial vehicle physics butt joint network deployment, four angles in side set up laser positioning device 11, utilize laser positioning device 11, but the large-scale cluster of multimachine butt joint constitution each other. Be equipped with data and energy transmission channel 10 in interfacing apparatus 9, utilize the logic control brain that the cluster formed to realize energy management behind the network deployment, what for example the network deployment partial unmanned aerial vehicle unit carried is the reserve energy, provide other task unmanned aerial vehicle as the supply unit, still can close the driving system of partial redundant unmanned aerial vehicle unit in the network deployment, the solar energy film of expansion shrink at its hexagon head utilizes the real-time supply energy of solar energy, thereby the task standby when realizing the long voyage of whole cluster.
The side of hexagonal head frame 3 still is equipped with fusion sensor/antenna 5 for unmanned aerial vehicle data acquisition, receiving and dispatching.
As shown in fig. 5, 3 of 25 unmanned aerial vehicle units (carrying different task units required for completing tasks) are firstly combined to form small assemblies through small-range physical docking, then on the basis, the rest unmanned aerial vehicle units are subjected to large-scale integrated networking, and a combined unmanned aerial vehicle cluster is formed through physical docking, namely the unmanned aerial vehicle assembly, some units carrying energy loads can be utilized inside the assembly to supply other task unmanned aerial vehicles, in order to realize long-time task standby, the power system of the partially redundant unmanned aerial vehicle units in the networking can be closed, the solar film which is expanded and contracted at the hexagonal head of the power system is utilized for on-site standby charging through real-time energy, the unmanned aerial vehicles are separated and released to execute tasks after being charged, and the whole cluster task standby time is prolonged.
Claims (6)
- The utility model provides an kinds of physics combination formula unmanned aerial vehicle cluster, its characterized in that forms by many unmanned aerial vehicle units physics combination, the unmanned aerial vehicle unit includes hexagon head frame, casing, coaxial bispin wing, take off and land skid and modularization task unit, hexagon head frame passes through the support frame and fixes the casing at the frame center, the take off and land skid is installed to the casing below, and coaxial bispin wing is connected at the casing top, the setting of modularization task unit is in chassis bottom, each limit of hexagon head frame all is equipped with interfacing apparatus, utilizes this interfacing apparatus to realize the physics combination of many unmanned aerial vehicle units.
- 2. The physically combined drone cluster of claim 1, wherein a retractable solar membrane is provided within the hexagonal head frame.
- 3. The physically combined drone cluster of claim 1, wherein the hexagonal head frame has integrated sensors/antennas on its sides for drone data acquisition, transceiving.
- 4. The physically combined unmanned aerial vehicle cluster of claim 1, wherein a power module, an energy storage module, a processing module and a communication module are arranged in the housing, the power module is used for providing power for taking off, landing and flying of the unmanned aerial vehicle, the energy storage module is used for storing electric energy for the power module and also used for storing electric energy converted from light energy when the solar film is unfolded for power generation, the processing module is used for managing and controlling other modules, and the communication module is used for data transceiving and transmitting.
- 5. The physically combined drone cluster of claim 1, wherein the drone stand-alone is purely electrically driven.
- 6. The physically combined drone cluster of claim 1, wherein the docking device has data and power transmission channels.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201822053723.4U CN210000581U (en) | 2018-12-07 | 2018-12-07 | physical combined unmanned aerial vehicle cluster |
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| CN201822053723.4U CN210000581U (en) | 2018-12-07 | 2018-12-07 | physical combined unmanned aerial vehicle cluster |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113220012A (en) * | 2021-04-06 | 2021-08-06 | 中国电子科技集团公司电子科学研究院 | Integrated cabin section for swarm unmanned aerial vehicle and swarm unmanned aerial vehicle |
| CN114275155A (en) * | 2021-11-30 | 2022-04-05 | 金陵科技学院 | Modular unmanned aerial vehicle and unmanned aerial vehicle electric quantity sharing system |
-
2018
- 2018-12-07 CN CN201822053723.4U patent/CN210000581U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113220012A (en) * | 2021-04-06 | 2021-08-06 | 中国电子科技集团公司电子科学研究院 | Integrated cabin section for swarm unmanned aerial vehicle and swarm unmanned aerial vehicle |
| CN114275155A (en) * | 2021-11-30 | 2022-04-05 | 金陵科技学院 | Modular unmanned aerial vehicle and unmanned aerial vehicle electric quantity sharing system |
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Address after: Nanchang high tech Industrial Development Zone, Jiangxi Province Patentee after: JIANGXI HONGDU AVIATION INDUSTRY GROUP Co.,Ltd. Address before: 330000 Jiangxi city in Nanchang Province, the new bridge box 460 box 5001 Patentee before: JIANGXI HONGDU AVIATION INDUSTRY GROUP Co.,Ltd. |