CN216509173U - Centralized transmitting and recycling cabin for unmanned aerial vehicle cluster - Google Patents
Centralized transmitting and recycling cabin for unmanned aerial vehicle cluster Download PDFInfo
- Publication number
- CN216509173U CN216509173U CN202220345438.3U CN202220345438U CN216509173U CN 216509173 U CN216509173 U CN 216509173U CN 202220345438 U CN202220345438 U CN 202220345438U CN 216509173 U CN216509173 U CN 216509173U
- Authority
- CN
- China
- Prior art keywords
- unmanned aerial
- aerial vehicle
- beacon
- cabin body
- hole
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Images
Landscapes
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The utility model provides a concentrated transmission recovery cabin for unmanned aerial vehicle crowd, relates to unmanned aerial vehicle technical field, including the recovery module of the cabin body, at least one emission module and supporting emission module quantity, the cabin body is equipped with a set of hole that is used for placing unmanned aerial vehicle, emission module is including the fixer that is used for fixed unmanned aerial vehicle and the catapult that is used for popping out unmanned aerial vehicle, the hole department at the cabin body is installed respectively to fixer and catapult, retrieve the infrared camera that the module includes four at least infrared beacons, GPS location beacon and is used for discerning infrared beacon, the periphery in the hole is installed to infrared beacon annular array, GPS location beacon is installed in the cabin body, infrared camera installs the below at unmanned aerial vehicle. The utility model has simple structure and high automation degree, greatly provides the control force of the unmanned aerial vehicle group, improves the take-off success rate, improves the recovery precision and greatly reduces the take-off and landing accidents caused by disordered management of the unmanned aerial vehicle group.
Description
Technical Field
The application relates to the technical field of unmanned aerial vehicles, in particular to a centralized launching recovery cabin for an unmanned aerial vehicle cluster.
Background
The unmanned aerial vehicle has wide application, low cost and higher efficiency; no casualty risk; the life ability is strong, the maneuverability is good, the use is convenient, the device plays an extremely important role in modern war and has a wider prospect in the civil field.
Unmanned aerial vehicles increasingly adopt a cluster mode to exist, and are used for tasks such as area search, plant protection operation, topographic survey.
However, the prior art has shortcomings with respect to centralized management of a drone cluster.
In the prior art, a piece of open ground or a platform is usually provided for an unmanned aerial vehicle group to take off and land, and the control mode is too loose, and the problems of unsmooth taking off or overlarge landing position deviation and the like often occur.
SUMMERY OF THE UTILITY MODEL
In order to solve among the prior art management and control mode too loose, and often can appear taking off not smoothly or landing position deviation too big scheduling problem, this application provides a concentrated transmission recovery cabin for unmanned aerial vehicle crowd. The following technical scheme is adopted:
the utility model provides a concentrated transmission recovery cabin for unmanned aerial vehicle crowd, includes the recovery module of the cabin body, at least one emission module and supporting emission module quantity, the cabin body is equipped with a set of hole that is used for placing unmanned aerial vehicle, emission module is including the fixer that is used for fixed unmanned aerial vehicle and the catapult that is used for popping out unmanned aerial vehicle, the hole department at the cabin body is installed respectively to fixer and catapult, retrieve the infrared camera that the module includes four at least infrared beacons, GPS location beacon and is used for discerning infrared beacon, the periphery in the hole is installed to infrared beacon annular array, GPS location beacon installs in the cabin internally, infrared camera installs the below at unmanned aerial vehicle.
According to the technical scheme, in the recovery state, the unmanned aerial vehicles are respectively positioned in the holes of the cabin body, the landing gear of the unmanned aerial vehicle is grabbed by the fixing device, the ejector is in the retraction state, and the infrared beacon and the GPS positioning beacon are respectively in the closing state;
when the unmanned aerial vehicle takes off and launches, the fixer releases the undercarriage of the unmanned aerial vehicle, the propeller of the unmanned aerial vehicle is started, then the catapult is catapulted to assist the unmanned aerial vehicle to take off, and the catapult retracts again after taking off is completed;
when unmanned aerial vehicle retrieves, infrared beacon and GPS location beacon are opened, and unmanned aerial vehicle's flight control system acquires GPS location beacon's GPS signal to fly to the cabin body, when being close to the cabin body, infrared camera starts the accurate position who acquires infrared beacon, thereby obtains the accurate position of landing point, falls back to appointed downthehole, and unmanned aerial vehicle closes, and the fixer restarts and grasps unmanned aerial vehicle's undercarriage.
Optionally, the hole is circular and can pass through unmanned aerial vehicle.
Through above-mentioned technical scheme, adopt the circular port, make things convenient for unmanned aerial vehicle's transmission and recovery more.
Optionally, the fixer includes base and at least one electronic clamping jaw, base fixed mounting is in the hole department of the cabin body, electronic clamping jaw is installed on the base, and when unmanned aerial vehicle descends and accomplishes, electronic clamping jaw's claw is grabbed unmanned aerial vehicle's undercarriage.
Through above-mentioned technical scheme, when needing fixed unmanned aerial vehicle, the start-up of electronic clamping jaw can be grabbed unmanned aerial vehicle's undercarriage.
Optionally, the catapult includes box body, first electro-magnet, second electro-magnet, a pair of linear guide, launches board and electromagnet controller, box body fixed mounting is in the hole department of the cabin body, the bottom at the box body is installed to first electro-magnet, a pair of linear guide's track is installed respectively on the lateral wall of box body, the both ends of launching the board are connected respectively and are installed on a pair of linear guide's slider to can reciprocate along with the slider, the lower surface at launching the board is installed to the second electro-magnet, the switch and the magnetic pole of first electro-magnet and second electro-magnet are controlled respectively to the electromagnet controller.
According to the technical scheme, when the unmanned aerial vehicle needs to be launched, the electromagnet controller respectively electrifys the first electromagnet and the second electromagnet, and the magnetic poles of the contact surfaces of the first electromagnet and the second electromagnet are the same, so that the second electromagnet is repelled by the first electromagnet to move upwards, the catapulting plate is driven to move upwards to catapult the unmanned aerial vehicle, and the action of catapulting the unmanned aerial vehicle is completed;
after ejection is finished, the electromagnet controller respectively controls the first electromagnet and the second electromagnet to be powered off, so that the second electromagnet falls back to be close to the first electromagnet, and the ejection plate retracts.
Optionally, a chip-based control main board is further provided, and the control main board is respectively in communication interconnection with the fixer, the ejector, the infrared beacon, the GPS positioning beacon and the flight control system of the unmanned aerial vehicle.
Through above-mentioned technical scheme, the electronic clamping jaw switching of control mainboard control fixer, control through control electromagnet controller control catapult ejection plate pop out and retract, control opening and closing of infrared beacon and GPS location beacon respectively to through the flying control system communication interconnection with unmanned aerial vehicle guide unmanned aerial vehicle take off and retrieve.
In summary, the present application includes at least one of the following beneficial technical effects:
the centralized launching and recycling cabin for the unmanned aerial vehicle group, provided by the utility model, has the advantages of simple structure and high automation degree, greatly provides the management and control force of the unmanned aerial vehicle group, improves the launching success rate, improves the recycling accuracy, and greatly reduces the launching and landing accidents caused by disordered management of the unmanned aerial vehicle group.
Drawings
FIG. 1 is a schematic diagram of the unmanned aerial vehicle of the present invention in a post-launch configuration;
FIG. 2 is a schematic structural diagram of the launch and recovery state of the UAV of the present invention;
FIG. 3 is a schematic view of the fastener of the present invention;
FIG. 4 is a schematic view of the ejector of the present invention;
FIG. 5 is a schematic diagram of the electrical principles of the present invention;
description of reference numerals: 1. a cabin body; 11. a hole; 2. a holder; 21. a base; 22. an electric jaw; 3. an ejector; 31. a box body; 32. a first electromagnet; 33. a second electromagnet; 34. a pair of linear guide rails; 35. ejecting a plate; 36. an electromagnet controller; 4. an infrared beacon; 5. a GPS positioning beacon; 6. an infrared camera for identifying an infrared beacon; 7. and controlling the main board.
Detailed Description
The present application is described in further detail below with reference to fig. 1-5.
The embodiment of the application discloses a centralized emission recovery cabin for an unmanned aerial vehicle cluster.
Referring to fig. 1-5, a concentrated transmission recovery cabin for unmanned aerial vehicle cluster, including cabin body 1, the recovery module of at least one emission module and supporting emission module quantity, cabin body 1 is equipped with a set of hole 11 that is used for placing unmanned aerial vehicle, emission module is including the fixer 2 that is used for fixed unmanned aerial vehicle and the catapult 3 that is used for popping out unmanned aerial vehicle, hole 11 department at cabin body 1 is installed respectively to fixer 2 and catapult 3, recovery module includes at least four infrared beacon 4, GPS location beacon 5 and the infrared camera 6 that is used for discerning infrared beacon, the periphery at hole 11 is installed to infrared beacon 4 annular array, GPS location beacon 5 is installed in cabin body 1, infrared camera 6 installs the below at unmanned aerial vehicle.
In a recovery state, the unmanned aerial vehicles are respectively positioned in the holes 11 of the cabin body 1, the landing gear of the unmanned aerial vehicles is grasped by the fixator 2, the catapult 3 is in a retraction state, and the infrared beacon 4 and the GPS positioning beacon 5 are respectively in a closing state;
when the unmanned aerial vehicle takes off and launches, the fixing device 2 releases the undercarriage of the unmanned aerial vehicle, the propeller of the unmanned aerial vehicle is started, then the catapult 3 is catapulted to assist the unmanned aerial vehicle to take off, and the catapult 3 retracts again after taking off is finished;
when unmanned aerial vehicle retrieves, infrared beacon 4 and GPS location beacon 5 are opened, and unmanned aerial vehicle's flight control system acquires GPS location beacon 5's GPS signal to fly to cabin body 1, when being close to cabin body 1, infrared camera 6 starts the accurate position of acquireing infrared beacon 4, thereby obtains the accurate position of landing point, falls back to appointed hole 11 in, and unmanned aerial vehicle closes, and 2 restarts of fixer grasp unmanned aerial vehicle's undercarriage.
Adopt the circular port, make things convenient for unmanned aerial vehicle's transmission and recovery more.
The fixer 2 includes base 21 and at least one electronic clamping jaw 22, and base 21 fixed mounting is in the hole 11 department of cabin body 1, and electronic clamping jaw 22 is installed on base 21, and when the unmanned aerial vehicle descends and accomplishes, and the undercarriage of unmanned aerial vehicle is grabbed to the claw of electronic clamping jaw 22.
When needing fixed unmanned aerial vehicle, electronic clamping jaw 22 starts can grasp unmanned aerial vehicle's undercarriage.
The ejector 3 comprises a box body 31, a first electromagnet 32, a second electromagnet 33, a pair of linear guide rails 34, an ejection plate 35 and an electromagnet controller 36, wherein the box body 31 is fixedly installed at the hole 11 of the cabin body 1, the first electromagnet 32 is installed at the bottom of the box body 31, the rails of the pair of linear guide rails 34 are respectively installed on the side wall of the box body 31, two ends of the ejection plate 35 are respectively connected and installed on the sliding blocks of the pair of linear guide rails 34 and can move up and down along with the sliding blocks, the second electromagnet 33 is installed on the lower surface of the ejection plate 35, and the electromagnet controller 36 respectively controls the on-off and magnetic poles of the first electromagnet 32 and the second electromagnet 33.
When the unmanned aerial vehicle needs to be launched, the electromagnet controller 36 respectively electrifys the first electromagnet 32 and the second electromagnet 33, and the magnetic poles of the contact surfaces of the first electromagnet 32 and the second electromagnet 33 are the same, so that the second electromagnet 33 is repelled by the first electromagnet 32 to move upwards, the catapulting plate 35 is driven to move upwards to catapult the unmanned aerial vehicle, and the action of catapulting the unmanned aerial vehicle is completed;
after the ejection is completed, the electromagnet controller 36 controls the first electromagnet 32 and the second electromagnet 33 to be powered off, respectively, so that the second electromagnet 33 falls back to be adjacent to the first electromagnet 32, and the ejection plate 35 retracts.
And a control mainboard 7 based on a chip, wherein the control mainboard 7 is respectively communicated and interconnected with the fixer 2, the ejector 3, the infrared beacon 4, the GPS positioning beacon 5 and a flight control system of the unmanned aerial vehicle.
The control mainboard 7 controls the opening and closing of the electric clamping jaw 22 of the fixer 2, controls the ejection and retraction of the ejection plate 35 of the ejector 3 through the control electromagnet controller 36, respectively controls the opening and closing of the infrared beacon 4 and the GPS positioning beacon 5, and guides the take-off and the recovery of the unmanned aerial vehicle through the communication and interconnection with the flight control system of the unmanned aerial vehicle.
The implementation principle of the centralized transmitting and recycling cabin for the unmanned aerial vehicle cluster is as follows:
in a recovery state, the unmanned aerial vehicles are respectively positioned in the holes 11 of the cabin body 1, the undercarriage of the unmanned aerial vehicle is held by the electric clamping jaws 22 of the fixator 2, the electromagnet controller 36 respectively controls the first electromagnet 32 and the second electromagnet 33 to be powered off, the second electromagnet 33 falls back to be close to the first electromagnet 32, the ejection plate 35 is in a retraction state, and the control main board 7 respectively controls the infrared beacon 4 and the GPS positioning beacon 5 to be in a closing state;
when the unmanned aerial vehicle takes off and launches, the electric clamping jaw 22 of the fixer 2 releases the landing gear of the unmanned aerial vehicle, the propeller of the unmanned aerial vehicle is started, then the main board 7 is controlled to respectively electrify the first electromagnet 32 and the second electromagnet 33 through the electromagnet controller 36, and the magnetic poles of the contact surfaces of the first electromagnet 32 and the second electromagnet 33 are the same, so that the second electromagnet 33 is repelled by the first electromagnet 32 to move upwards, the catapulting plate 35 is driven to move upwards to catapult the unmanned aerial vehicle, the action of catapulting the unmanned aerial vehicle is completed, the unmanned aerial vehicle is assisted to complete the takeoff, after the takeoff is completed, the electromagnet controller 36 respectively controls the first electromagnet 32 and the second electromagnet 33 to be powered off, the second electromagnet 33 falls back to be close to the first electromagnet 32, and the catapulting plate 35 retracts again;
when unmanned aerial vehicle retrieves, control mainboard 7 controls infrared beacon 4 and GPS location beacon 5 respectively and opens, unmanned aerial vehicle's flight control system acquires GPS location beacon 5's GPS signal, thereby fly to cabin body 1, when being close to cabin body 1, infrared camera 6 starts the accurate position of acquireing infrared beacon 4, thereby obtain the accurate position of landing point, fall back to appointed hole 11 in, unmanned aerial vehicle closes, electronic clamping jaw 22 restart of fixer 2 grasps unmanned aerial vehicle's undercarriage, unmanned aerial vehicle's recovery has been accomplished promptly.
The above embodiments are preferred embodiments of the present application, and the protection scope of the present application is not limited by the above embodiments, so: all equivalent changes made according to the structure, shape and principle of the present application shall be covered by the protection scope of the present application.
Claims (5)
1. A centralized launch recovery pod for a fleet of drones, comprising: including the recovery module of cabin body (1), at least one emission module and supporting emission module quantity, the cabin body (1) is equipped with a set of hole (11) that are used for placing unmanned aerial vehicle, emission module is including fixer (2) that are used for fixed unmanned aerial vehicle and catapult (3) that are used for popping out unmanned aerial vehicle, hole (11) department in the cabin body (1) are installed respectively to fixer (2) and catapult (3), the recovery module includes at least four infrared beacon (4), GPS location beacon (5) and infrared camera (6) that are used for discerning infrared beacon, the periphery in hole (11) is installed to infrared beacon (4) annular array, install in cabin body (1) GPS location beacon (5), the below at unmanned aerial vehicle is installed in infrared camera (6).
2. The centralized launch recovery trunk for a drone swarm of claim 1, wherein: hole (11) are circular, and can pass through unmanned aerial vehicle.
3. The centralized launch recovery trunk for a drone swarm of claim 1, wherein: fixer (2) include base (21) and at least one electronic clamping jaw (22), base (21) fixed mounting is in hole (11) department of cabin body (1), electronic clamping jaw (22) are installed on base (21), and when unmanned aerial vehicle descends and accomplishes, the claw of electronic clamping jaw (22) grasps unmanned aerial vehicle's undercarriage.
4. The centralized launch recovery pod for an unmanned aerial vehicle cluster of claim 1, wherein: ejector (3) include box body (31), first electro-magnet (32), second electro-magnet (33), a pair of linear guide (34), launch board (35) and electromagnet controller (36), box body (31) fixed mounting is in hole (11) department of the cabin body (1), the bottom at box body (31) is installed in first electro-magnet (32), the track of a pair of linear guide (34) is installed respectively on the lateral wall of box body (31), launch the both ends of board (35) and connect respectively and install on the slider of a pair of linear guide (34) to can reciprocate along with the slider, the lower surface at launching board (35) is installed in second electro-magnet (33), electromagnet controller (36) control the switch and the magnetic pole of first electro-magnet (32) and second electro-magnet (33) respectively.
5. A centralized launch recovery pod for an unmanned aerial vehicle fleet according to any one of claims 1 to 4, wherein: and the control main board (7) is based on a chip, and the control main board (7) is respectively communicated and interconnected with the fixer (2), the ejector (3), the infrared beacon (4), the GPS positioning beacon (5) and the flight control system of the unmanned aerial vehicle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220345438.3U CN216509173U (en) | 2022-02-21 | 2022-02-21 | Centralized transmitting and recycling cabin for unmanned aerial vehicle cluster |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220345438.3U CN216509173U (en) | 2022-02-21 | 2022-02-21 | Centralized transmitting and recycling cabin for unmanned aerial vehicle cluster |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216509173U true CN216509173U (en) | 2022-05-13 |
Family
ID=81519104
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202220345438.3U Active CN216509173U (en) | 2022-02-21 | 2022-02-21 | Centralized transmitting and recycling cabin for unmanned aerial vehicle cluster |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216509173U (en) |
-
2022
- 2022-02-21 CN CN202220345438.3U patent/CN216509173U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US11858631B2 (en) | Aerial launch and/or recovery for unmanned aircraft with submersible devices, and associated systems and methods | |
| US10933996B2 (en) | Release and capture of a fixed-wing aircraft | |
| AU2017200817B2 (en) | Magnetic orientation detent | |
| CN105270627A (en) | Two-unmanned-aircraft system capable of being charged in air and improving endurance capability | |
| CN205060016U (en) | Charge in air and promote two unmanned aerial vehicle systems of duration | |
| CN105059550A (en) | Double unmanned aerial vehicle with improved endurance | |
| EP3201088A1 (en) | Transportable ground station for an unmanned aerial vehicle | |
| TWI676578B (en) | Take-off device and method for unmanned aircraft without landing gear | |
| CN205168905U (en) | Stationary vane aerial survey unmanned aerial vehicle | |
| CN106849224A (en) | A kind of unmanned plane is continued a journey system automatically | |
| CN109094807A (en) | A kind of unmanned plane battery change system | |
| CN106915452A (en) | A kind of composite aircraft landing system | |
| CN202879795U (en) | Multipurpose unmanned plane with flexible ram-type parawings | |
| CN216509173U (en) | Centralized transmitting and recycling cabin for unmanned aerial vehicle cluster | |
| CN204056287U (en) | A kind of autonomous flight is without active force unmanned plane | |
| CN108082400A (en) | Aerial photography aircraft airplane parking area waterborne | |
| CN113212782B (en) | Ultrashort-distance landing system of fixed-wing unmanned aerial vehicle | |
| CN109159768A (en) | A kind of unmanned plane battery change method | |
| CN104192295B (en) | A kind of autonomous flight is without active force unmanned plane and flying method thereof | |
| CN214930648U (en) | Unmanned aerial vehicle moves aircraft nest in air | |
| CN109502024A (en) | A kind of aircraft and unmanned aerial vehicle | |
| CN109334973A (en) | A kind of the first visual angle aircraft using tail sitting posture VTOL fixed-wing | |
| CZ2017418A3 (en) | Unmanned vehicle | |
| CN216546710U (en) | Delivery device based on unmanned aerial vehicle | |
| CN210455225U (en) | Unmanned aerial vehicle machine carries pylon |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |