CN111186579B - Swarm unmanned aerial vehicle deployment system based on air carrier throwing - Google Patents
Swarm unmanned aerial vehicle deployment system based on air carrier throwing Download PDFInfo
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- CN111186579B CN111186579B CN202010054567.2A CN202010054567A CN111186579B CN 111186579 B CN111186579 B CN 111186579B CN 202010054567 A CN202010054567 A CN 202010054567A CN 111186579 B CN111186579 B CN 111186579B
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- unmanned aerial
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D5/00—Aircraft transported by aircraft, e.g. for release or reberthing during flight
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
Abstract
The invention discloses a swarm unmanned aerial vehicle deployment system based on air carrier throwing, which relates to the field of unmanned aerial vehicles and comprises an air carrier and a throwing hanging box positioned in an independent inner cabin, wherein a machine body of the air carrier consists of a plurality of independent inner cabins arranged side by side, and the bottom of the independent inner cabin is provided with a baffle plate capable of opening and closing; and every independent under deck all is equipped with one and throws and hangs the case, throw the bottom opening that hangs the case, throw and hang the incasement and be equipped with unmanned aerial vehicle unit link plate, unmanned aerial vehicle unit link plate lower surface is equipped with automatically controlled couple, it is equipped with the unmanned aerial vehicle unit to hang on the automatically controlled couple. And the inner top surface of the independent inner cabin is provided with a fixing bayonet for fixing the top of the throwing hanging box. The invention realizes low-cost rapid deployment of the bee colony, reduces the safety risk of the whole system deployment, and has higher application and practical value.
Description
Technical Field
The invention relates to the field of unmanned aerial vehicles, in particular to a swarm unmanned aerial vehicle deployment system based on air carrier throwing.
Background
The quick and batch deployment of bee colony unmanned aerial vehicle is the important influence factor of bee colony unmanned aerial vehicle performance combat power, and the domestic main mode that is used for bee colony unmanned aerial vehicle space-based deployment at present has two kinds: one is a launching mode based on a slide rail, a launching bracket and a launcher combination device, such as an unmanned aerial vehicle space-based launching device (publication number is CN108100287A) in the patent and an unmanned aerial vehicle space launching device (publication number is CN109263996A) in the patent; the other is a launching system based on a towing cable towing target, for example, an unmanned aerial vehicle space-based rapid launching device and method based on an aviation towing cable towing target system (publication No. CN 107792371A). The two modes can both meet the problems of rapid deployment and large quantity deployment of swarm unmanned aerial vehicles, but the technical requirements on the adapted swarm unmanned aerial vehicles are high, according to the principles of the 'unmanned aerial vehicle air-based launching device' and the 'swarm unmanned aerial vehicle air launching device' in the patents, the swarm unmanned aerial vehicles which are required to be adapted have the functions of folding before wingspan launching and rapid unfolding after launching, the technical process is close to the cruise missile technology, and the 'unmanned aerial vehicle air-based rapid launching device and method based on the aviation towing cable target system' require that the swarm unmanned aerial vehicles on the towing cables firstly have the explosion-proof function, the towing target system is not reusable, and the launching cost of the whole system is high.
As is known, swarm drones win the force of the mass, and can only exert the advantages of a distributed system at low cost. However, although the existing air-based deployment mode is theoretically feasible for rapidly deploying a plurality of swarm unmanned aerial vehicles, the deployment mode has corresponding requirements on the unmanned aerial vehicles, so that the manufacturing process and the standard of the swarm unmanned aerial vehicles are indirectly improved, and the corresponding manufacturing cost is also increased. Under the condition that the application quantity of future swarm unmanned aerial vehicles is large, the pressure of a user can be increased, the continuous application capacity is obviously weakened, obviously, the deployment mode which does not consider the requirement of adapting the low-cost swarm unmanned aerial vehicles does not have enough application value, and from the aspect, the existing three rapid deployment modes do not effectively solve the problems of rapid and batch deployment of the swarm unmanned aerial vehicles.
Disclosure of Invention
Aiming at the defects in the prior art, the invention aims to provide a swarm unmanned aerial vehicle deployment system based on air carrier throwing, which realizes low-cost and rapid swarm deployment, reduces the safety risk of the whole system deployment and has higher application and practical values.
In order to achieve the above purposes, the technical scheme adopted by the invention is as follows:
the aircraft body of the aircraft carrier consists of a plurality of independent inner cabins arranged side by side, and the bottoms of the independent inner cabins are openable baffles;
the throwing hanging box is located in the independent inner cabin, the throwing hanging box is arranged in each independent inner cabin, the bottom opening of the throwing hanging box is formed, an unmanned aerial vehicle unit hanging plate is arranged in the throwing hanging box, an electric control hook is arranged on the lower surface of the unmanned aerial vehicle unit hanging plate, and an unmanned aerial vehicle unit is hung on the electric control hook.
On the basis of the technical scheme, the inner top surface of the independent inner cabin is provided with a fixed bayonet used for fixing the top of the throwing hanging box, slide rails are arranged on two sides of the bottom of the independent inner cabin, the bottom of one side wall is located in the slide rail on one side of the bottom of the independent inner cabin, and the bottom of the other side wall is located in the slide rail on the other side of the bottom of the independent inner cabin.
On the basis of the technical scheme, the unmanned aerial vehicle unit link plate of the throwing hanging box is a plurality of, and parallel arrangement from top to bottom between a plurality of unmanned aerial vehicle unit link plates of the throwing hanging box, one end part activity of the unmanned aerial vehicle unit link plate is fixed on the lateral wall of the throwing hanging box, and the unmanned aerial vehicle unit link plate can rotate up and down around the end part.
On the basis of the technical scheme, be equipped with automatically controlled slow descending bearing on the lateral wall of the hanging case of jettisoning, unmanned aerial vehicle unit link plate is fixed in automatically controlled slow descending bearing with the fixed tip of jettisoning hanging case lateral wall activity, automatically controlled slow descending bearing is used for driving unmanned aerial vehicle unit link plate and carries out the tilting around this tip.
On the basis of the technical scheme, the electric sliding rail is vertically arranged on the side wall of the throwing hanging box, and the electric control slow-falling bearing is located on the electric sliding rail and can move up and down along the direction of the electric sliding rail.
On the basis of the technical scheme, the number of the unmanned aerial vehicle unit hanging plates at the same height in the throwing hanging box is two, and the unmanned aerial vehicle unit hanging plates at the same height are respectively movably fixed on two opposite side walls of the throwing hanging box.
On the basis of the technical scheme, the aircraft carrier is a self-rotary wing unmanned aerial vehicle.
On the basis of the technical scheme, the top of the unmanned aerial vehicle unit is provided with a hook interface used for being connected with an electric control hook.
On the basis of the technical scheme, the unmanned aerial vehicle unit is a multi-rotor unmanned aerial vehicle.
On the basis of the technical scheme, the independent inner cabins are cuboids, and the independent inner cabins are arranged side by side along the length direction of the aircraft carrier.
Compared with the prior art, the invention has the advantages that: the throwing hanging box adopts a low-cost box type design, can be conveniently configured on a modified unmanned aerial vehicle air carrier, supports batch or one-by-one release of suspended swarm unmanned aerial vehicle units, and supports reuse; the unmanned aerial vehicle unit can be configured into a cheap racing model, the rapid deployment of the whole system can completely realize unmanned deployment, a professional pilot and a high-performance weapon-level airplane are not required to be relied on, the safety risk of the deployment of the whole system is reduced while the low-cost rapid deployment of bee colonies is realized, and the unmanned aerial vehicle unit has high application and practical values.
Drawings
Fig. 1 is a schematic structural diagram of a swarm unmanned aerial vehicle deployment system based on aircraft carrier throwing in the embodiment of the invention;
FIG. 2 is a schematic structural diagram of a casting hanging box in the embodiment of the invention;
fig. 3 is a schematic structural diagram of an unmanned aerial vehicle unit according to an embodiment of the present invention;
FIG. 4 is a schematic view of an initial casting situation in an embodiment of the invention;
FIG. 5 is a schematic view of the lowest drone unit beginning to cast in an example of the invention;
fig. 6 is a schematic view illustrating that the lowermost unmanned aerial vehicle unit link plate starts to rotate in the embodiment of the invention;
fig. 7 is a schematic view illustrating a lowermost unmanned aerial vehicle unit link plate rotating to a vertical state in the embodiment of the present invention;
figure 8 is a schematic view of the start of the tossing of a penultimate drone unit in an example of the invention;
fig. 9 is a schematic view of the top drone unit beginning to cast in an example of the invention.
In the figure: 1-an air carrier, 2-a slide rail, 3-a fixed bayonet, 4-a baffle, 5-a throwing hanging box, 6-an electric slide rail, 7-an electric control slow descending bearing, 8-an unmanned aerial vehicle unit hanging plate, 9-an electric control hook, 10-an unmanned aerial vehicle unit and 11-a hook interface.
Detailed Description
The embodiment of the invention provides a swarm unmanned aerial vehicle deployment system based on air carrier throwing, which adopts a hanging mode, is convenient to throw and effectively reduces the deployment cost of swarm unmanned aerial vehicles. The present invention will be described in further detail with reference to the accompanying drawings and examples.
Referring to fig. 1, a swarm unmanned aerial vehicle deployment system based on air carrier throwing provided by the embodiment of the invention comprises an air carrier 1 and a throwing hanging box 5 located in an independent inner cabin.
The aircraft body of the aircraft carrier 1 consists of a plurality of independent inner cabins arranged side by side, and the bottoms of the independent inner cabins are retractable baffles 4. The independent inner cabins are cuboids, and the independent inner cabins are arranged side by side along the length direction of the aircraft carrier 1. The aircraft carrier 1 is a self-rotary wing unmanned aerial vehicle with the load larger than 130 kg. Baffle 4 of independent inner chamber bottom adopts the electric control mode control, and when unmanned aerial vehicle need release, baffle 4 is opened, otherwise is the closed condition, keeps the closure of whole organism. The interior top surface of independent inner deck is equipped with the fixed bayonet 3 that is used for fixed 5 tops of hanging case of jettisoning, and the bottom both sides of independent inner deck all are equipped with slide rail 2, and in the relative both sides wall of hanging case 5 of jettisoning, the bottom of a lateral wall is arranged in slide rail 2 of independent inner deck bottom one side, and the bottom of another lateral wall is arranged in slide rail 2 of independent inner deck bottom opposite side, through fixed bayonet 3 and slide rail 2, is convenient for jettison the loading of hanging case 5.
The main function of the casting hanging box 5 is to provide a stable hanging environment and controllable casting release conditions for the casting type swarm unmanned aerial vehicle unit 10, the casting hanging box 5 combines the task requirements through the automatic sensing of the flight state of the aircraft carrier 1 and the information synthesis of the swarm unmanned aerial vehicle unit 10, and the optimal casting release strategy is automatically planned, so that the swarm unmanned aerial vehicle needing to be released can be released in an operation airspace more safely, efficiently and quickly. The whole design size of a single throwing hanging box 5 is not more than 100 x 50cm, the weight is not more than 30kg, the system power consumption is not more than 200w, the single throwing hanging box can carry not less than 6 swarm unmanned aerial vehicle units 10 simultaneously, and the minimum throwing interval time is not less than 10 s. The throwing hanging box 5 on the aircraft carrier 1 can release a plurality of unmanned aerial vehicle units 10 simultaneously, also can release designated unmanned aerial vehicle units 10 in batches, and the throwing hanging box 5 can be reused for many times.
Referring to fig. 2, all being equipped with one in every independent interior cabin and throwing and hanging case 5, the bottom opening of throwing and hanging case 5 is equipped with unmanned aerial vehicle unit link plate 8 in throwing and hanging case 5, and unmanned aerial vehicle unit link plate 8 lower surface is equipped with automatically controlled couple 9, hangs on the automatically controlled couple 9 and is equipped with unmanned aerial vehicle unit 10. Unmanned aerial vehicle unit link plate 8 of the interior of box 5 is hung in the jettison is a plurality of, and throws and hang a plurality of unmanned aerial vehicle unit link plates 8 within the box 5 parallel arrangement from top to bottom, and on an end activity of unmanned aerial vehicle unit link plate 8 was fixed in the lateral wall of box 5 is hung in the jettison, and unmanned aerial vehicle unit link plate 8 can carry out the tilting around this tip. Be equipped with automatically controlled slow descending bearing 7 on the lateral wall of the hanging box 5 of jettisoning, the unmanned aerial vehicle unit link plate 8 is fixed in automatically controlled slow descending bearing 7 with the tip of 5 lateral walls activity of jettisoning hanging box, automatically controlled slow descending bearing 7 is used for driving unmanned aerial vehicle unit link plate 8 and carries out the tilting around this tip. An electric slide rail 6 is vertically arranged on the side wall of the throwing hanging box 5, and an electric control slow-falling bearing 7 is positioned on the electric slide rail 6 and can move up and down along the direction of the electric slide rail 6. Unmanned aerial vehicle unit link plate 8 on the same height in the case 5 is hung in the throwing is two, and unmanned aerial vehicle unit link plate 8 on the same height is movably fixed in respectively on the relative both sides wall of case 5 is hung in the throwing.
Referring to fig. 3, the drone unit 10 is a multi-rotor drone, and the top of the drone unit 10 is provided with a hook interface 11 for connection with an electronic control hook 9. The main cost of the unmanned aerial vehicle unit 10 in the embodiment of the invention is in the attachment of the communication link module, other components are configured in a lower level in the industry, the design of light weight and miniaturization is realized as much as possible, the cost is effectively reduced, the radar signal reflection area can be reduced, the survival probability is improved, and the distributed cooperative operation is completed. The wheelbase of the swarm unmanned aerial vehicle unit 10 is less than or equal to 450mm, the weight of the whole machine is less than or equal to 5kg, the endurance time is greater than or equal to 30min, the working altitude is greater than or equal to 8000m, the control radius is greater than or equal to 5km, the load capacity is greater than or equal to 1.2kg, the aerial unlocking stable height is less than or equal to 15m, the wind resistance level is greater than or equal to 4, the swarm unmanned aerial vehicle unit can be adapted to various load modules. The low-cost swarm unmanned aerial vehicle units 10 are mounted in different layers of the casting hanging boxes 5, and the casting hanging boxes 5 can be quickly placed in different independent inner cabins of the aircraft carrier 1.
The following describes the tossing process of the drone unit 10 in an embodiment of the present invention with reference to an example.
Referring to fig. 4, the unmanned aerial vehicle unit hanging plate 8 is kept parallel in an initial state when the unmanned aerial vehicle unit 10 is thrown; after the throwing is started, the hook interface 11 on the unmanned aerial vehicle unit 10 at the lowest layer in the throwing hanging box 5 is disconnected with the electric control hook 9, and the throwing is started, which is shown in fig. 5; after the lowest unmanned aerial vehicle unit 10 finishes throwing, the lowest unmanned aerial vehicle unit hanging plate 8 starts to rotate, and the view is shown in fig. 6; when the unmanned aerial vehicle unit hanging plate 8 at the lowest layer rotates to be in a vertical state, see fig. 7; the electric control slow descending bearing 7 drives the unmanned aerial vehicle unit hanging plate 8 on the penultimate layer to move downwards along the electric slide rail 6, moves to a position close to the hatch, and throws the unmanned aerial vehicle unit 10 after the movement is finished, and is shown in fig. 8; after the unmanned aerial vehicle units 10 on the penultimate floor finish throwing, the unmanned aerial vehicle units 10 on the uppermost floor start throwing according to the above throwing mode, and as shown in fig. 9, after all the unmanned aerial vehicle units 10 finish throwing, the baffles 4 of the independent inner cabins are closed.
According to the swarm unmanned aerial vehicle deployment system based on the air carrier throwing, the throwing hanging box 5 adopts a low-cost box type design, can be conveniently configured on the modified unmanned aerial vehicle air carrier 1, supports batch or one-by-one release of the suspended swarm unmanned aerial vehicle units 10, and supports reuse; the unmanned aerial vehicle unit 10 can be configured into a cheap racing model, the rapid deployment of the whole system can completely realize unmanned deployment, a professional pilot and a high-performance weapon-level airplane are not required to be relied on, the safety risk of the deployment of the whole system is reduced while the low-cost rapid deployment of bee colonies is realized, and the unmanned aerial vehicle unit has high application and practical values.
The present invention is not limited to the above-described embodiments, and it will be apparent to those skilled in the art that various modifications and improvements can be made without departing from the principle of the present invention, and such modifications and improvements are also considered to be within the scope of the present invention. Those not described in detail in this specification are within the skill of the art.
Claims (9)
1. The utility model provides a bee colony unmanned aerial vehicle deploys system based on air carrier is jettisoned, its characterized in that includes:
the aircraft body of the aircraft carrier (1) consists of a plurality of independent inner cabins arranged side by side, and the bottoms of the independent inner cabins are retractable baffles (4);
the throwing hanging boxes (5) are positioned in the independent inner cabins, each independent inner cabin is provided with one throwing hanging box (5), the bottom of each throwing hanging box (5) is provided with an opening, an unmanned aerial vehicle unit hanging plate (8) is arranged in each throwing hanging box (5), the lower surface of each unmanned aerial vehicle unit hanging plate (8) is provided with an electric control hook (9), and an unmanned aerial vehicle unit (10) is hung on each electric control hook (9);
the unmanned aerial vehicle unit hanging plates (8) in the throwing hanging box (5) are arranged in a plurality of modes, the unmanned aerial vehicle unit hanging plates (8) in the throwing hanging box (5) are arranged in parallel from top to bottom, one end part of each unmanned aerial vehicle unit hanging plate (8) is movably fixed on the side wall of the throwing hanging box (5), and the unmanned aerial vehicle unit hanging plates (8) can rotate up and down around the end part.
2. The drone deployment system for bee colonies based on aircraft carrier jettisoning of claim 1, wherein: the inner top surface of the independent inner cabin is provided with a fixed bayonet (3) used for fixing the top of the throwing hanging box (5), the two sides of the bottom of the independent inner cabin are provided with slide rails (2), in the two opposite side walls of the throwing hanging box (5), the bottom of one side wall is positioned in the slide rail (2) on one side of the bottom of the independent inner cabin, and the bottom of the other side wall is positioned in the slide rail (2) on the other side of the bottom of the independent inner cabin.
3. The drone deployment system for bee colonies based on aircraft carrier jettisoning of claim 1, wherein: be equipped with automatically controlled slow descending bearing (7) on the lateral wall of the hanging case of jettisoning (5), unmanned aerial vehicle unit link plate (8) and the fixed tip of the hanging case of jettisoning (5) lateral wall activity are fixed in automatically controlled slow descending bearing (7), automatically controlled slow descending bearing (7) are used for driving unmanned aerial vehicle unit link plate (8) and carry out the tilting around this tip.
4. The drone deployment system for bee colonies based on aircraft carrier jettisoning of claim 3, wherein: the side wall of the casting hanging box (5) is vertically provided with an electric sliding rail (6), and the electric control slow descending bearing (7) is located on the electric sliding rail (6) and can move up and down along the direction of the electric sliding rail (6).
5. The drone deployment system for bee colony based on aircraft carrier jettison of claim 4, characterized in that: unmanned aerial vehicle unit link plate (8) on the same height in throwing hanging case (5) are two, and unmanned aerial vehicle unit link plate (8) on the same height are movably fixed in respectively on the relative both sides wall of throwing hanging case (5).
6. The drone deployment system for bee colonies based on aircraft carrier jettisoning of claim 1, wherein: the aircraft carrier (1) is a self-rotary wing unmanned aerial vehicle.
7. The drone deployment system for bee colonies based on aircraft carrier jettisoning of claim 1, wherein: the top of the unmanned aerial vehicle unit (10) is provided with a hook interface (11) used for being connected with the electric control hook (9).
8. The drone deployment system for bee colonies based on aircraft carrier jettisoning of claim 1, wherein: the unmanned aerial vehicle unit (10) is a multi-rotor unmanned aerial vehicle.
9. The drone deployment system for bee colonies based on aircraft carrier jettisoning of claim 1, wherein: the independent inner cabins are cuboid, and the independent inner cabins are arranged side by side along the length direction of the aircraft carrier (1).
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010054567.2A CN111186579B (en) | 2020-01-17 | 2020-01-17 | Swarm unmanned aerial vehicle deployment system based on air carrier throwing |
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| CN202010054567.2A CN111186579B (en) | 2020-01-17 | 2020-01-17 | Swarm unmanned aerial vehicle deployment system based on air carrier throwing |
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| CN111186579A CN111186579A (en) | 2020-05-22 |
| CN111186579B true CN111186579B (en) | 2021-04-09 |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN113879536A (en) * | 2021-10-25 | 2022-01-04 | 北京航空航天大学 | Multilayer primary and secondary formula unmanned vehicles winding and unwinding devices |
| CN113895623A (en) * | 2021-10-27 | 2022-01-07 | 桂林电子科技大学 | Unmanned aerial vehicle is patrolled and examined in monitoring |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| FR2953809B1 (en) * | 2009-12-16 | 2012-04-06 | Mbda France | LOADING AND LOADING SYSTEM FOR TRANSPORT PLANE |
| CN106347664A (en) * | 2016-11-29 | 2017-01-25 | 海鹰航空通用装备有限责任公司 | Leaflet spreading device for multi-rotor unmanned aerial vehicle and use method of leaflet spreading device |
| US10065717B1 (en) * | 2017-09-14 | 2018-09-04 | SparkCognition, Inc. | Autonomous vessel for unmanned combat aerial vehicle (UCAV) carrier operations |
| CN109263996A (en) * | 2018-10-23 | 2019-01-25 | 西北工业大学 | A kind of bee colony unmanned plane aerial-launcher |
| CN109747827B (en) * | 2018-12-27 | 2022-05-17 | 中国航空工业集团公司西安飞机设计研究所 | Multi-group rectangular slide rail type unmanned aerial vehicle launching device and launching method |
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Application publication date: 20200522 Assignee: Woke Kongtian Technology (Suzhou) Co.,Ltd. Assignor: Hubei woke Intelligent Technology Co.,Ltd. Contract record no.: X2021420000024 Denomination of invention: A bee swarm UAV deployment system based on air carrier throwing Granted publication date: 20210409 License type: Exclusive License Record date: 20210913 |
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