CN216805810U - Net-catching type unmanned aerial vehicle with counter-braking equipment - Google Patents
Net-catching type unmanned aerial vehicle with counter-braking equipment Download PDFInfo
- Publication number
- CN216805810U CN216805810U CN202220364834.0U CN202220364834U CN216805810U CN 216805810 U CN216805810 U CN 216805810U CN 202220364834 U CN202220364834 U CN 202220364834U CN 216805810 U CN216805810 U CN 216805810U
- Authority
- CN
- China
- Prior art keywords
- net
- unmanned aerial
- aerial vehicle
- transmitter
- buckle
- 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
- 230000005540 biological transmission Effects 0.000 claims abstract description 21
- 101100495256 Caenorhabditis elegans mat-3 gene Proteins 0.000 description 3
- 230000005284 excitation Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 230000005611 electricity Effects 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 239000012634 fragment Substances 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 230000002452 interceptive effect Effects 0.000 description 1
- 210000001503 joint Anatomy 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
Images
Landscapes
- Forklifts And Lifting Vehicles (AREA)
Abstract
The utility model discloses a net-catch type unmanned aerial vehicle with a counter-braking device. The three-optical pod is mounted on the lower side of the front end of the unmanned aerial vehicle body, the net-capture transmitter is provided with a first quick-release mechanism, and the net-capture transmitter is mounted on a hanging support plate at the bottom of the unmanned aerial vehicle body through the first quick-release mechanism; the net catches the transmitter and includes every single move rotation portion and transmission portion, rotates the transmitter angular adjustment of portion drive net catching through every single move, later catches the net through transmission portion transmission from net under-deck, catches "low little" unmanned aerial vehicle in certain distance department, and the capture range is great, has good anti-system ability.
Description
Technical Field
The utility model relates to a net-capture type unmanned aerial vehicle, in particular to a net-capture type unmanned aerial vehicle with a counter-braking device, and belongs to the technical field of unmanned aerial vehicles.
Background
An unmanned aerial vehicle is a flying body that flies by remote control without a human being riding or flies from a main location along a predetermined route, and has been mainly used for military purposes; because the consumption-level unmanned aerial vehicle is low in cost, easy to obtain and simple to control, and enters the market along with numerous unmanned aerial vehicle manufacturers, the commercial unmanned aerial vehicle can quickly go deep into the civil field, the number of users is gradually increased, the supervision difficulty is high, the commercial unmanned aerial vehicle can be easily utilized by lawbreakers, and if some lawbreakers use the unmanned aerial vehicle to steal and spy commercial secrets and the like, great pressure is brought to security and confidential work. In the international field, relevant precautionary measures have been taken for the black flying phenomenon of the unmanned aerial vehicle, however, the supervision of the domestic unmanned aerial vehicle is still in a blank state, and if corresponding precautionary control measures are not taken, the illegal unmanned aerial vehicle can cause great hidden troubles for aerial supervision and aerial safety; so that the anti-unmanned aerial vehicle technology is also in urgent need of development.
In recent years, the number of the unmanned aerial vehicles with low speed and small size shows an explosive growth trend, and a large number of unmanned aerial vehicles fly black to bring about extremely serious low-altitude safety problems. In order to effectively standardize the low-altitude flight of the unmanned aerial vehicle and guarantee public safety, China pays attention to the technical research work of the anti-unmanned aerial vehicle. The conventional firepower hitting hit rate is low, the cost effectiveness ratio is high, and therefore the net catching type unmanned aerial vehicle counter-braking equipment is provided and has the advantages of being low in cost effectiveness ratio, large in catching range, high in fault tolerance rate, high in hit rate and the like.
Among the prior art, because conventional firepower strikes the hit rate low and cost-effectiveness ratio high, and the fragment easily causes the damage to personnel or object around when unmanned aerial vehicle crashes. Unmanned aerial vehicle counter-braking equipment with large capture range, high hit rate and low danger is required.
Disclosure of Invention
The utility model aims to solve the problems in the prior art and provides a novel net-capture type unmanned aerial vehicle with a counter-braking device.
In order to achieve the above object, the present invention adopts the following technical solutions:
a net-catch type unmanned aerial vehicle with a counter-braking device comprises an unmanned aerial vehicle body, three-light pods and a net-catch transmitter; the three-light pod is installed on the lower side of the front end of the unmanned aerial vehicle body, the net-capture transmitter is provided with a first quick-release mechanism, and the net-capture transmitter is installed on a hanging support plate at the bottom of the unmanned aerial vehicle body through the first quick-release mechanism; the net catching transmitter comprises a pitching rotating part and a transmitting part, the pitching rotating part drives the net catching transmitter to adjust the angle, and then the transmitting part transmits the catching net to complete reverse catching.
Preferably, the hanging support plate comprises a hanging support plate bottom plate, a hanging support plate top plate and a PCB (printed circuit board) arranged between the hanging support plate bottom plate and the hanging support plate top plate, the first quick-release mechanism is a buckle type quick-release mechanism and comprises buckle buttons, buckle push rods, rotating connecting rods and buckle springs, the buckle buttons are fixedly arranged on the hanging support plate bottom plate, the number of the buckle push rods and the number of the rotating connecting rods are two, the rotating connecting rods are connected with the buckle push rods through one ends of positioning pins, the other ends of the rotating connecting rods are connected with the buckle buttons, and the buckle springs are arranged inside the buckle buttons.
Preferably, aforementioned net catches transmitter includes stores pylon, transmitter base, high definition digtal camera, every single move rotation portion and transmitting part, every single move rotation portion sets up on the transmitter base, the transmitter base is installed in the inside of stores pylon, the stores pylon is installed on hanging the support plate, high definition digtal camera passes through threaded connection in the below of transmitter base, transmitting part and every single move rotation portion fixed connection, rotate the portion drive transmitting part through every single move and go on pitching the regulation to reach suitable transmission angle.
More preferably, aforementioned every single move rotation portion includes power transmission structure, bearing and bearing frame, power transmission structure with transmitter base drive connection drives the transmitter base and carries out the every single move and rotate, bearing and bearing frame fixed connection are provided with 2 relatively, 2 the bearing is fixed on the two relative inner walls of stores pylon, bearing frame one side and transmitter base pass through the fix with screw, give a pivoted strong point of transmitter base through bearing and bearing frame, make things convenient for the transmitter base to carry out the every single move rotation.
Preferably again, aforementioned power transmission structure includes steering wheel, steering wheel support, steering wheel connection piece, steering wheel arm and bulb pull rod, the steering wheel passes through the steering wheel leg joint on the stores pylon, one side drive connection is kept away from transmitter base through screw and bearing frame to steering wheel connection piece one end, and the other end passes through the drive with the bulb pull rod and is connected, the bulb pull rod with the steering wheel arm drive is connected, the steering wheel arm is connected in the output pivot of steering wheel. When the steering engine rotates, the output rotating shaft drives the steering engine arm, the ball head pull rod and the steering engine connecting sheet to move, then the steering engine connecting sheet drives the bearing seat to rotate, the bearing seat drives the emitter base to rotate, and the net cabin is installed on the emitter base, so that the control of the net cabin pitch angle can be realized.
Further preferably, the launching part comprises a miniature gas generator, a net cabin and a launching tube, the launching tube is mounted in the launching base through a second quick-release mechanism, the launching tube and the net cabin are fixed through threads, and the miniature gas generator is fixedly connected with the launching tube through threads. The miniature gas generator is ignited by electric excitation, the catching net is launched from the net cabin, and the target is caught.
Still further preferably, the second quick release mechanism comprises a rotary buckle and a spring, the rotary buckle and the spring are both installed in the emitter base, and the rotary buckle and the spring are elastically connected. The rotation buckle rotates along the rotating shaft due to the elasticity of the spring, and meanwhile, the rotation buckle cannot rotate all the time due to the limitation of the transmitter base, so that the protruding structure of the rotation buckle is just clamped in the clamping groove of the transmitting tube, and the transmitting tube and the transmitter base are fixed.
Still further preferably, an intelligent recognition device is arranged inside the unmanned aerial vehicle body, and the intelligent recognition device is respectively in electric signal connection with the unmanned aerial vehicle body, the three-optical pod and the net capture transmitter and performs information interactive transmission through the intelligent recognition device.
And, aforementioned unmanned aerial vehicle body is a many rotor unmanned aerial vehicle.
The utility model has the advantages that:
(1) according to the net capture type unmanned aerial vehicle with the reverse control equipment, the capture net is launched from the net cabin through the launching part, the low-slow small unmanned aerial vehicle is captured at a certain distance, the capture range is large, and the reverse control capacity is good; when the steering engine of the unmanned aerial vehicle rotates, the output rotating shaft drives the steering engine arm, the ball head pull rod and the steering engine connecting sheet to move, then the steering engine connecting sheet drives the bearing seat to rotate, the bearing seat drives the emitter base to rotate, and the net cabin is arranged on the emitter base, so that the control of the pitch angle of the net cabin can be better realized;
(2) according to the net-capture type unmanned aerial vehicle with the reverse braking device, the launching tube is installed in the launcher base through the second quick-release mechanism, the rotating buckle rotates along the rotating shaft due to the elasticity of the spring, and meanwhile, the rotating buckle cannot rotate all the time due to the limiting of the launcher base, so that the protruding structure of the rotating buckle is just clamped in the clamping groove of the launching tube, the launching tube and the launcher base can be fixed, and the operation is convenient.
Drawings
FIG. 1 is a schematic overall structure of an embodiment of the present invention;
FIG. 2 is an exploded view of the structure of one embodiment of the present invention;
FIG. 3 is an exploded view of a first quick release mechanism according to an embodiment of the present invention;
fig. 4 is a cross-sectional view of an emitter base according to an embodiment of the present invention.
The meaning of the reference symbols in the figures:
1-a multi-rotor unmanned aerial vehicle body, 2-a net catching launcher, 3-a launching tube, 4-a three-light pod, 5-an intelligent recognition module, 6-a miniature gas generator, 7-a steering engine connecting sheet, 8-a steering engine arm, 9-a steering engine bracket, 10-a ball pull rod, 11-a steering engine, 12-a high definition camera, 13-a net cabin, 14-a bearing seat, 15-a bearing, 16-a hanging rack, 17-a hanging board, 171-a hanging board bottom board, 172-a hanging board top board, 173-a PCB, 18-a spring, 19-a rotating buckle, 20-a launcher base, 21-a buckle button, 22-a buckle push rod, 23-a rotating connecting rod and 24-a buckle spring.
Detailed Description
The utility model is described in detail below with reference to the figures and the embodiments.
In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on those shown in the drawings, and are used only for convenience in describing the present invention and for simplicity in description, and do not indicate or imply that the referenced devices or elements must have a particular orientation, be constructed and operated in a particular orientation, and thus, are not to be construed as limiting the present invention. Furthermore, the terms "first," "second," and the like are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
The net-capture unmanned aerial vehicle with the counter-braking device is shown in fig. 1 and fig. 2, and comprises a multi-rotor unmanned aerial vehicle body 1, a three-light pod 4 and a net-capture transmitter 2. Wherein, three smooth pod 4 are installed in the front end downside of many rotor unmanned aerial vehicle body 1, are provided with first quick detach mechanism on net catches transmitter 2, and net catches formula transmitter and installs on the carry board 17 of many rotor unmanned aerial vehicle body 1 bottom through first quick detach mechanism. This carry board 17 is including carry board bottom plate 171, carry board roof 172 and the PCB173 of setting between carry board bottom plate 171 and carry board roof 172, first quick detach mechanism is buckle formula quick detach mechanism, including buckle button 21, buckle push rod 22, rotating connecting rod 23, buckle spring 24, buckle button 21 fixed mounting is on carry board bottom plate 171, buckle push rod 22 and rotating connecting rod 23 homogeneous phase are provided with two relatively, rotating connecting rod 23 passes through locating pin one end and is connected with buckle push rod 22, the other end is connected with buckle button 21, buckle spring 24 installs the inside at buckle button 21. By pressing the snap button 24, the quick assembly and disassembly of the net-catching transmitter is realized. The net capture emitter 2 comprises a pitching rotating part and an emitting part, the pitching rotating part drives the net capture emitter 2 to adjust the angle, and then the emitting part emits the capture net to complete reverse capture. And, the inside intelligent recognition device that is provided with of many rotor unmanned aerial vehicle body 1, intelligent recognition device respectively with many rotor unmanned aerial vehicle body 1, three optical pod 4 and net catch 2 electricity signal connection of transmitter, carry out information interaction transmission through intelligent recognition device.
In this embodiment, as shown in fig. 2, in order to reach suitable transmission angle with the transmission portion adjustment, this unmanned aerial vehicle's net capture transmitter 2 includes stores pylon 16, transmitter base 20, high definition digtal camera 12, every single move rotation portion and transmission portion, every single move rotation portion sets up on transmitter base 20, transmitter base 20 installs in the inside of stores pylon 16, stores pylon 16 is installed on hanging support plate 17, high definition digtal camera 12 passes through threaded connection in the below of transmitter base 20, transmission portion and every single move rotation portion fixed connection, it adjusts to pitch to rotate the portion drive transmission portion through every single move, in order to reach suitable transmission angle.
Wherein, the every single move rotation portion for realizing the every single move regulation includes power transmission structure, bearing 15 and bearing frame 14, power transmission structure and transmitter base 20 drive connection, drive transmitter base 20 carries out the every single move rotation, bearing 15 and bearing frame 14 fixed connection are provided with 2 relatively, 2 bearing 15 are fixed on the two relative inner walls of stores pylon 16, bearing frame 14 one side and transmitter base 20 pass through the fix with screw, give transmitter base 20 a pivoted strong point through bearing 15 and bearing frame 14, make things convenient for transmitter base 20 to carry out the every single move rotation. The power transmission structure comprises a steering engine 11, a steering engine support 9, a steering engine connecting piece 7, a steering engine arm 8 and a ball head pull rod 10, wherein the steering engine 11 is connected to a hanging rack 16 through the steering engine support 9, one end of the steering engine connecting piece 7 is in driving connection with one side, far away from a transmitter base 20, of a bearing seat 14 through a screw, the other end of the steering engine connecting piece is in driving connection with the ball head pull rod 10, the ball head pull rod 10 is in driving connection with the steering engine arm 8, and the steering engine arm 8 is connected to an output rotating shaft of the steering engine 11. When steering wheel 11 rotates, the output rotating shaft drives rudder horn 8, bulb pull rod 10 and steering wheel connection piece 7 to move, and then steering wheel connection piece 7 drives bearing frame 14 to rotate, and bearing frame 14 drives transmitter base 20 to rotate, because net cabin 13 is installed on transmitter base 20, so can realize the control to net cabin 13 angle of pitch.
In this embodiment, the launching part for realizing launching the capture net comprises a micro gas generator 6, a net cabin 13 and a launching tube 3, the launching tube 3 is installed in a launcher base 20 through a second quick-release mechanism, the launching tube 3 is fixedly connected with the net cabin 13 through threads, and the micro gas generator 6 is fixedly connected with the launching tube 3 through threads. The micro gas generator 6 is ignited by electric excitation, and the catching net is launched from the net cabin 13 to catch the target.
In the embodiment, the second quick release mechanism comprises a rotating buckle 19 and a spring 18, the rotating buckle 19 is connected with the emitter base 20 from the rear of the emitter base 20 through a screw, the spring 18 is installed in the emitter base 20 from the side, and the rotating buckle 19 is elastically connected with the spring 18. The rotation buckle 19 is because of the elasticity of the spring 18, when rotating along the rotating shaft, and simultaneously, because the spacing messenger of the emitter base 20 rotates the buckle 19 and can not rotate all the time, the protruding structure of the rotation buckle 19 can just be blocked in the clamping groove of the emitter tube 3, and then the emitter tube 3 and the emitter base 20 are fixed.
For further explanation of the present embodiment, the following is further detailed with reference to the workflow of the present embodiment:
in the course of the work, the user installs net cabin 13 in transmitter base 20 through the second quick detach mechanism of launching tube 3, installs net catch transmitter 2 in many rotor unmanned aerial vehicle body 1 bottom through the first quick detach mechanism of hanging support plate 17. Treat unmanned aerial vehicle ready back, the user controls unmanned aerial vehicle flight destination point, after unmanned aerial vehicle flies to the operation place, three light nacelle 4 begin to search for the unmanned aerial vehicle target, and intelligent recognition module 5 receives the image information that three light nacelle 4 sent in real time through prior art, after treating the discovery target, transmits the unmanned aerial vehicle with the target for unmanned aerial vehicle's position to aim through high definition digtal camera 12. According to the target position information transmitted by the intelligent recognition module 5, the unmanned aerial vehicle automatically adjusts the position and the posture of the unmanned aerial vehicle, controls the pitching angle of the net capture emitter 2 to track and aim the target, and excites the miniature gas generator 6 in the net capture emitter 2 to pop out the capture net to complete the capture of the target.
In summary, according to the net-capture type unmanned aerial vehicle with the reverse braking device, the launching tube 3 is installed in the launcher base 20 through the second quick-release mechanism, the rotating buckle 19 rotates along the rotating shaft due to the elastic force of the spring 18, and meanwhile, the rotating buckle 19 cannot rotate all the time due to the limiting of the launcher base 20, so that the protruding structure of the rotating buckle 19 is just clamped in the clamping groove of the launching tube 3, the launching tube 3 and the launcher base 20 can be fixed, and the operation is convenient. When the steering engine 11 of the unmanned aerial vehicle rotates, the output rotating shaft drives the steering engine arm 8, the ball head pull rod 10 and the steering engine connecting sheet 7 to move, then the steering engine connecting sheet 7 drives the bearing seat 14 to rotate, the bearing seat 14 drives the emitter base 20 to rotate, and the net cabin 13 is mounted on the emitter base 20, so that the pitch angle of the net cabin 13 can be better controlled; simultaneously, catch the net through launching of launching portion in from net cabin 13, catch "low slow little" unmanned aerial vehicle in certain distance department, the capture range is great, has good resistance ability.
In the description of the present invention, it should be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
In the description herein, references to the description of the term "one embodiment," "some embodiments," "an example," "a specific example," or "some examples," etc., mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the utility model. In this specification, the schematic representations of the terms used above do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
The foregoing illustrates and describes the principles, general features, and advantages of the present invention. It should be understood by those skilled in the art that the above embodiments do not limit the present invention in any way, and all technical solutions obtained by using equivalent alternatives or equivalent variations fall within the scope of the present invention.
Claims (9)
1. A net-catch type unmanned aerial vehicle with a counter-braking device is characterized by comprising an unmanned aerial vehicle body, a three-light nacelle and a net-catch transmitter;
the three-optical pod is mounted on the lower side of the front end of the unmanned aerial vehicle body, the net-capture transmitter is provided with a first quick-release mechanism, and the net-capture transmitter is mounted on a hanging support plate at the bottom of the unmanned aerial vehicle body through the first quick-release mechanism;
the net catching transmitter comprises a pitching rotating part and a transmitting part, the pitching rotating part drives the net catching transmitter to adjust the angle, and then the transmitting part transmits the catching net to complete reverse catching.
2. The net-capture unmanned aerial vehicle with the countering device as defined in claim 1, wherein the net-capture transmitter comprises a hanger, a transmitter base, a high-definition camera, a pitching rotating part and a transmitting part, the pitching rotating part is arranged on the transmitter base, the transmitter base is mounted inside the hanger, the hanger is mounted on a hanging support plate, the high-definition camera is connected below the transmitter base through threads, and the transmitting part is fixedly connected with the pitching rotating part.
3. The net-capture unmanned aerial vehicle with the countering device as defined in claim 2, wherein the pitching rotating part comprises a power transmission structure, bearings and bearing seats, the power transmission structure is in driving connection with the emitter base, the bearings and the bearing seats are fixedly connected and are oppositely provided with 2, the 2 bearings are fixed on two opposite inner walls of the hanging rack, and one side of the bearing seat is fixed with the emitter base through screws.
4. The net-catching unmanned aerial vehicle with the reverse braking device as claimed in claim 3, wherein the power transmission structure comprises a steering engine, a steering engine support, a steering engine connecting piece, a steering engine arm and a ball head pull rod, the steering engine is connected to the hanging rack through the steering engine support, one end of the steering engine connecting piece is in driving connection with one side, away from the emitter base, of the bearing seat through a screw, the other end of the steering engine connecting piece is in driving connection with the ball head pull rod, the ball head pull rod is in driving connection with the steering engine arm, and the steering engine arm is connected to an output rotating shaft of the steering engine.
5. The net capture type unmanned aerial vehicle with the counter-braking device as claimed in claim 2, wherein the launching part comprises a micro gas generator, a net cabin and a launching tube, the launching tube is mounted in the launching base through a second quick release mechanism, the launching tube and the net cabin are fixed through threads, and the micro gas generator is fixedly connected with the launching tube through threads.
6. The net capture type unmanned aerial vehicle with the counter-braking device as claimed in claim 5, wherein the second quick release mechanism comprises a rotating buckle and a spring, the rotating buckle and the spring are both installed in the launcher base, and the rotating buckle and the spring are elastically connected.
7. The net capture type unmanned aerial vehicle with the reverse braking device according to claim 1, wherein the hanging plate comprises a hanging plate bottom plate, a hanging plate top plate and a PCB arranged between the hanging plate bottom plate and the hanging plate top plate, the first quick-release mechanism is a buckle type quick-release mechanism and comprises buckle keys, buckle push rods, two rotating connecting rods and buckle springs, the buckle keys are fixedly arranged on the hanging plate bottom plate, the two rotating connecting rods are arranged oppositely, one end of each rotating connecting rod is connected with the corresponding buckle push rod through a positioning pin, the other end of each rotating connecting rod is connected with the corresponding buckle key, and the corresponding buckle spring is arranged inside the corresponding buckle key.
8. The net capture type unmanned aerial vehicle with the countering device is characterized in that an intelligent recognition device is arranged inside the unmanned aerial vehicle body, and the intelligent recognition device is in electrical signal connection with the unmanned aerial vehicle body, the three-optical pod and the net capture transmitter respectively.
9. A net arresting drone with a countering device according to claim 1, characterized in that the drone body is a multi-rotor drone.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220364834.0U CN216805810U (en) | 2022-02-21 | 2022-02-21 | Net-catching type unmanned aerial vehicle with counter-braking equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220364834.0U CN216805810U (en) | 2022-02-21 | 2022-02-21 | Net-catching type unmanned aerial vehicle with counter-braking equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216805810U true CN216805810U (en) | 2022-06-24 |
Family
ID=82041340
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202220364834.0U Active CN216805810U (en) | 2022-02-21 | 2022-02-21 | Net-catching type unmanned aerial vehicle with counter-braking equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216805810U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116534268A (en) * | 2023-05-19 | 2023-08-04 | 上海战航智能科技有限公司 | Embedded aircraft arresting system and method for self-adaptive vector adjustment recovery |
-
2022
- 2022-02-21 CN CN202220364834.0U patent/CN216805810U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116534268A (en) * | 2023-05-19 | 2023-08-04 | 上海战航智能科技有限公司 | Embedded aircraft arresting system and method for self-adaptive vector adjustment recovery |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP2772429A1 (en) | Four-rotor aircraft | |
| US10293929B2 (en) | Multicopter-assisted system and method for launching and retrieving a fixed-wing aircraft | |
| US10696388B2 (en) | Multicopter-assisted system and method for launching and retrieving a fixed-wing aircraft | |
| CN107187605B (en) | A kind of multifunctional patrol drone and control method for agriculture and forestry | |
| WO2014067224A1 (en) | Quadcopter | |
| CN213323741U (en) | Cloud platform, camera carrier and movable platform | |
| CN214451849U (en) | A police drone with anti-crash function | |
| CN216805810U (en) | Net-catching type unmanned aerial vehicle with counter-braking equipment | |
| CN208882106U (en) | A kind of multi-rotor unmanned aerial vehicle with smog identification function | |
| CN212966773U (en) | Unmanned aerial vehicle is used in outdoor teaching with display device | |
| CN108082478B (en) | Early warning type unmanned aerial vehicle monitoring and investigation system | |
| CN110422339B (en) | Method for assembling coaxial double-rotor unmanned aerial vehicle | |
| CN219044414U (en) | Rotatable camera cradle head capable of carrying common unmanned aerial vehicle | |
| CN109278981B (en) | Miniature foldable three-dimensional live-action modeling unmanned aerial vehicle | |
| CN113401330B (en) | Collapsible miniature rotor unmanned aerial vehicle | |
| CN218258719U (en) | Multi-rotor unmanned aerial vehicle platform | |
| CN211107949U (en) | Lantern unmanned aerial vehicle | |
| CN207631524U (en) | Automatic safety device and hitching type electric self-service machine | |
| CN216943519U (en) | Unmanned aerial vehicle rack mechanism | |
| CN220010100U (en) | Small and miniature reconnaissance unmanned aerial vehicle | |
| CN217969940U (en) | Take many rotor unmanned aerial vehicle of parachute | |
| CN215436913U (en) | A protection gasbag subassembly that falls for many rotor unmanned aerial vehicle | |
| CN221843619U (en) | Bird repelling device for airport | |
| CN220924530U (en) | Shock attenuation nacelle cloud platform structure | |
| CN119218456B (en) | A UAV for panoramic imaging with a distributed array |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |