CN112977820A - Unmanned aerial vehicle intercepting device - Google Patents
Unmanned aerial vehicle intercepting device Download PDFInfo
- Publication number
- CN112977820A CN112977820A CN202110281419.9A CN202110281419A CN112977820A CN 112977820 A CN112977820 A CN 112977820A CN 202110281419 A CN202110281419 A CN 202110281419A CN 112977820 A CN112977820 A CN 112977820A
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- China
- Prior art keywords
- aerial vehicle
- unmanned aerial
- vehicle body
- detachably connected
- intercepting
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- 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.)
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- 150000001875 compounds Chemical class 0.000 claims abstract description 12
- 230000007306 turnover Effects 0.000 claims description 27
- 238000005192 partition Methods 0.000 claims description 8
- 210000002414 leg Anatomy 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/20—Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H11/00—Defence installations; Defence devices
- F41H11/02—Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Radar, Positioning & Navigation (AREA)
- General Engineering & Computer Science (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The invention discloses an unmanned aerial vehicle intercepting device, wherein the wireless radar, the compound eye camera and the high-frequency generator are arranged on the mounting rack, the adjustable storage rack is detachably connected with the unmanned aerial vehicle body, the transmitting device is arranged at one end of the adjustable storage rack away from the unmanned aerial vehicle body, the intercepting net body is arranged in the transmitting device, when the unmanned aerial vehicle body flies in the air, whether an illegal unmanned aerial vehicle exists in the air or not is monitored through the infinite radar and the compound eye camera, when the illegal unmanned aerial vehicle is monitored, the high-frequency transmitter interferes the signal of the illegal unmanned aerial vehicle, thereby the trace of the illegal unmanned aerial vehicle can be followed, and finally the angle of the launching device is adjusted through the adjustable containing frame, so that the launching device aims at the illegal unmanned aerial vehicle, therefore, the interception net body at the transmitting position of the transmitting device intercepts the illegal unmanned aerial vehicle.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicle intercepting devices, in particular to an unmanned aerial vehicle intercepting device.
Background
Along with the quick update of unmanned aerial vehicle technique, the unmanned aerial vehicle quantity that explosive growth has also brought huge supervision blind area, because limit is fuzzy relatively between civilian unmanned aerial vehicle and the model aeroplane and model ship, supervise in the aspect of the sale is relatively weak, leads to unable molecule wantonly to fly, brings huge potential safety hazard.
Disclosure of Invention
The invention aims to provide an unmanned aerial vehicle intercepting device, and aims to solve the technical problems that in the prior art, the boundary between a civil unmanned aerial vehicle and a model airplane is relatively fuzzy, the supervision in the aspect of sales is weak, so that a person cannot arbitrarily fly, and huge potential safety hazards are brought.
In order to achieve the purpose, the unmanned aerial vehicle intercepting device comprises an unmanned aerial vehicle body, an undercarriage, wing rods, propellers, a capturing device and an intercepting device, wherein the unmanned aerial vehicle body is detachably connected with the undercarriage and is positioned above the undercarriage, the plurality of wing rods are uniformly arranged on the periphery of the unmanned aerial vehicle body, the propellers are arranged at one ends, away from the unmanned aerial vehicle body, of the wing rods, the tops of the unmanned aerial vehicle body are provided with the capturing device, a containing cavity is formed in the unmanned aerial vehicle body, the intercepting device is arranged in the containing cavity, the capturing device comprises a mounting frame, a wireless radar, a compound eye camera and a high-frequency transmitter, the mounting frame is detachably connected with the unmanned aerial vehicle body and is positioned above the unmanned aerial vehicle body, and the wireless radar, the propeller, the capturing device and the intercepting device are arranged on the mounting frame, Compound eye camera with high frequency generator, intercepting device accomodates frame, emitter and interception dictyosome with adjustable, accomodate the frame with adjustable with the connection can be dismantled to the unmanned aerial vehicle organism, and be located accomodate the intracavity, accomodate the frame with adjustable and keep away from the one end of unmanned aerial vehicle organism is provided with emitter, be provided with in the emitter the interception dictyosome.
Wherein the adjustable storage rack comprises a connecting plate, a base, a rotating device, a rotating plate, an electric push rod, a placing plate, a turnover seat and a turnover device, the connecting plate is detachably connected with the unmanned aerial vehicle body, and is positioned in the containing cavity, the base is detachably connected with the connecting plate, one end of the base, which is far away from the connecting plate, is provided with a groove, the rotating device is arranged in the groove, the output end of the rotating device is provided with the rotating plate, the mounting end of the electric push rod is detachably connected with the rotating plate, the pushing end of the electric push rod is detachably connected with the placing plate, the placing plate is provided with a turnover frame and the turnover device, the turnover seat is movably connected with the turnover frame, the output end of the turnover device is matched with the turnover seat, and the emission device is arranged on the turnover seat.
The rotating device comprises a first motor and a first reduction gearbox, the first motor is detachably connected with the base, the first reduction gearbox is arranged at the output end of the first motor, the rotating plate is arranged at the output end of the first reduction gearbox, a partition plate is arranged inside the base and located between the first motor and the first reduction gearbox, and the first reduction gearbox is detachably connected with the partition plate.
The turnover device comprises a second motor, a second reduction gearbox, a rotating shaft and a clamping tooth, the second motor is detachably connected with the placing plate, the second reduction gearbox is arranged at the output end of the second motor, the rotating shaft is arranged at the output end of the second reduction gearbox, the clamping tooth is arranged at one end, away from the second reduction gearbox, of the rotating shaft, a clamping groove is formed in the turnover seat, and the clamping tooth is matched with the clamping groove.
Wherein, every the outside of screw all is provided with screw anticollision frame.
Wherein, every screw anticollision frame all includes go-between, bracing piece and protection ring, the go-between cover is established the outside of wing pole, the protection ring cover is established the outside of screw, the outer wall of go-between with evenly be provided with many between the inner wall of protection ring the bracing piece, every the bracing piece all is the slope structure setting.
The invention has the beneficial effects that: the wireless radar, the compound eye camera and the high-frequency generator are arranged on the mounting rack, the adjustable storage rack is detachably connected with the unmanned aerial vehicle body, the transmitting device is arranged at one end of the adjustable storage rack away from the unmanned aerial vehicle body, the intercepting net body is arranged in the transmitting device, when the unmanned aerial vehicle body flies in the air, whether an illegal unmanned aerial vehicle exists in the air or not is monitored through the infinite radar and the compound eye camera, when the illegal unmanned aerial vehicle is monitored, the high-frequency transmitter interferes the signal of the illegal unmanned aerial vehicle, thereby the trace of the illegal unmanned aerial vehicle can be followed, and finally the angle of the launching device is adjusted through the adjustable containing frame, so that the launching device aims at the illegal unmanned aerial vehicle, therefore, the interception net body at the transmitting position of the transmitting device intercepts the illegal unmanned aerial vehicle.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the drawings without creative efforts.
Fig. 1 is a schematic structural diagram of an unmanned aerial vehicle intercepting apparatus of the present invention.
Fig. 2 is a schematic structural view of an adjustable storage rack of the present invention.
Fig. 3 is a sectional view of the internal structure of fig. 2 taken along line a-a of the present invention.
Fig. 4 is a schematic view of the internal structure of the telescopic rod of the present invention.
1-unmanned aerial vehicle body, 2-landing gear, 3-wing rod, 4-propeller, 5-mounting rack, 6-wireless radar, 7-compound eye camera, 8-high frequency transmitter, 9-adjustable storage rack, 10-transmitter, 11-interception net body, 12-connecting plate, 13-base, 14-rotator, 15-rotator, 16-electric push rod, 17-placing plate, 18-turning seat, 19-turning device, 20-turning frame, 21-first motor, 22-first reduction gearbox, 23-partition plate, 24-second motor, 25-second reduction gearbox, 26-rotating shaft, 27-latch, 28-propeller anti-collision frame, 29-connecting ring, 30-supporting rod, 31-protection ring, 32-mounting plate, 33-telescopic rod, 34-supporting foot, 35-outer rod, 36-inner rod and 37-spring.
Detailed Description
Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are illustrative and intended to be illustrative of the invention and are not to be construed as limiting the invention.
In the description of the present invention, it is to be understood that the terms "length", "width", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on the orientations or positional relationships illustrated in the drawings, and are used merely for convenience in describing the present invention and for simplicity in description, and do not indicate or imply that the devices or elements referred to must have a particular orientation, be constructed in a particular orientation, and be operated, and thus, are not to be construed as limiting the present invention. Further, in the description of the present invention, "a plurality" means two or more unless specifically defined otherwise.
Referring to fig. 1 to 4, the invention provides an unmanned aerial vehicle intercepting device, which comprises an unmanned aerial vehicle body 1, an undercarriage 2, wing rods 3, a propeller 4, a capturing device and an intercepting device, wherein the unmanned aerial vehicle body 1 is detachably connected with the undercarriage 2 and is positioned above the undercarriage 2, a plurality of wing rods 3 are uniformly arranged around the unmanned aerial vehicle body 1, one end of each wing rod 3, which is far away from the unmanned aerial vehicle body, is provided with the propeller 4, the top of the unmanned aerial vehicle body 1 is provided with the capturing device, a containing cavity is arranged inside the unmanned aerial vehicle body 1, the intercepting device is arranged in the containing cavity, the capturing device comprises a mounting frame 5, a wireless radar 6, a compound eye camera 7 and a high-frequency transmitter 8, the mounting frame 5 is detachably connected with the unmanned aerial vehicle body 1 and is positioned above the unmanned aerial vehicle body 1, be provided with on the mounting bracket 5 wireless radar 6 compound eye camera 7 with high frequency generator, intercepting device accomodates frame 9, emitter 10 and interception dictyosome 11 including adjustable, accomodate frame 9 with the connection can be dismantled to unmanned aerial vehicle organism 1 to be located accomodate the intracavity, accomodate frame 9 with adjustable and keep away from the one end of unmanned aerial vehicle organism 1 is provided with emitter 10, be provided with in the emitter 10 interception dictyosome 11.
In the embodiment, the mounting frame 5 is detachably connected with the unmanned aerial vehicle body 1, the wireless radar 6, the compound eye camera 7 and the high-frequency generator are arranged on the mounting frame 5, the intercepting device comprises an adjustable storage frame 9, a transmitting device 10 and an intercepting net body 11, the adjustable storage frame 9 is detachably connected with the unmanned aerial vehicle body 1 and is positioned in the storage cavity, the transmitting device 10 is arranged at one end of the adjustable storage frame 9, which is far away from the unmanned aerial vehicle body 1, the intercepting net body 11 is arranged in the transmitting device 10, when the unmanned aerial vehicle body 1 flies in the air, whether an illegal unmanned aerial vehicle exists in the air is monitored through the infinite radar and the compound eye camera 7, after the illegal unmanned aerial vehicle is monitored, the signal of the illegal unmanned aerial vehicle is interfered through the high-frequency transmitter 8, so that the trace of the illegal unmanned aerial vehicle can follow, finally, the angle of the emitting device 10 is adjusted through the adjustable storage rack 9, so that the emitting device 10 aims at the illegal unmanned aerial vehicle, and the intercepting net body 11 intercepts the illegal unmanned aerial vehicle through the emitting position of the emitting device 10.
Further, the adjustable storage rack 9 comprises a connecting plate 12, a base 13, a rotating device 14, a rotating plate 15, an electric push rod 16, a placing plate 17, a turning seat 18 and a turning device 19, the connecting plate 12 is detachably connected with the unmanned aerial vehicle body 1 and is located inside the storage cavity, the base 13 is detachably connected with the connecting plate 12, a groove is formed in one end, away from the connecting plate 12, of the base 13, the rotating device 14 is arranged inside the groove, the rotating plate 15 is arranged at the output end of the rotating device 14, the mounting end of the electric push rod 16 is detachably connected with the rotating plate 15, the pushing end of the electric push rod 16 is detachably connected with the placing plate 17, a turning frame 20 and the turning device 19 are arranged on the placing plate 17, the turning seat 18 is movably connected with the turning frame 20, the output end of the turnover device 19 is matched with the turnover seat 18, and the launching device 10 is arranged on the turnover seat 18.
In this embodiment, the rotating device 14 drives the electric push rod 16 on the rotating disc to rotate, the electric push rod 16 drives the placing plate 17 to lift, and the overturning device 19 drives the reflecting device on the overturning seat 18 to overturn, so that the launching device 10 aims at the unmanned plane to be intercepted.
Further, the rotating device 14 comprises a first motor 21 and a first reduction gearbox 22, the first motor 21 is detachably connected with the base 13, the first reduction gearbox 22 is arranged at the output end of the first motor 21, the rotating plate 15 is arranged at the output end of the first reduction gearbox 22, a partition plate 23 is arranged inside the base 13, the partition plate 23 is located between the first motor 21 and the first reduction gearbox 22, and the first reduction gearbox 22 is detachably connected with the partition plate 23.
In this embodiment, the first motor 21 is started, and after the output power of the first motor 21 is reduced by the first reduction gearbox 22, the output end of the first reduction gearbox 22 drives the rotating disc to rotate slowly.
Further, the turnover device 19 includes a second motor 24, a second reduction gearbox 25, a rotation shaft 26 and a latch 27, the second motor 24 is detachably connected with the placing plate 17, the second reduction gearbox 25 is arranged at an output end of the second motor 24, the rotation shaft 26 is arranged at an output end of the second reduction gearbox 25, the latch 27 is arranged at one end, far away from the second reduction gearbox 25, of the rotation shaft 26, a clamping groove is formed in the turnover seat 18, and the latch 27 is matched with the clamping groove.
In this embodiment, the second motor 24 is started, and after the output power of the second motor 24 is reduced by the second reduction gearbox 25, the latch 27 on the rotating shaft 26 drives the overturning seat 18 to overturn.
Further, a propeller collision prevention frame 28 is provided outside each of the propellers 4.
In this embodiment, the propeller collision avoidance frame 28 prevents the propeller 4 from colliding with other flying objects in the air during the flight process, so that the unmanned aerial vehicle body 1 falls.
Further, every screw anticollision frame 28 all includes go-between 29, bracing piece 30 and protection ring 31, go-between 29 cover is established the outside of wing pole 3, protection ring 31 covers and establishes the outside of screw 4, go-between 29's outer wall with evenly be provided with many between the inner wall of protection ring 31 bracing piece 30, every bracing piece 30 all is the slope structure setting.
In this embodiment, the connection ring 29 and the protection ring 31 are both fixedly connected to the support rod 30, and are manufactured by using an integral molding technology, so that the structure is more firm, and during installation, the connection ring 29 is firstly sleeved outside the wing rod 3, and then the propeller 4 is installed, so that the protection ring 31 is located outside the propeller 4, and the propeller 4 is protected.
Further, undercarriage 2 includes two mounting panels 32, four telescopic links 33 and four supporting legss 34, two mounting panel 32 all with the connection can be dismantled to unmanned aerial vehicle organism 1, and be located unmanned aerial vehicle organism 1's bottom both sides, every the both ends of mounting panel 32 all are provided with two telescopic link 33, every bracing piece 30 is kept away from the one end of mounting panel 32 all is provided with supporting legss 34.
In this embodiment, when the unmanned aerial vehicle organism 1 bumps in the air and urgently forces to land, through the part is alleviated to telescopic link 33 unmanned aerial vehicle organism 1 drops the power that produces, thereby avoids unmanned aerial vehicle organism 1 receives comparatively serious damage.
Further, every telescopic link 33 all includes outer pole 35, interior pole 36 and spring 37, the one end of outer pole 35 with mounting panel 32 fixed connection, the other end of outer pole 35 is provided with the sliding tray, be provided with in the sliding tray spring 37, the one end of interior pole 36 with outer pole 35 sliding connection, and be located in the sliding tray, and with spring 37 laminates mutually, the other end of interior pole 36 with supporting legs 34 can dismantle the connection.
In this embodiment, when unmanned aerial vehicle organism 1 bumps in the air when promptly compelling to land, unmanned aerial vehicle organism 1 descends to the power that ground produced, through outer pole 35 transmit extremely interior pole 36's in-process, through spring 37 relieves partly, thereby avoids unmanned aerial vehicle organism 1 receives comparatively serious damage.
While the invention has been described with reference to a preferred embodiment, it will be understood by those skilled in the art that various changes in form and detail may be made therein without departing from the spirit and scope of the invention as defined by the appended claims.
Claims (6)
1. An intercepting device of an unmanned aerial vehicle is characterized in that,
the unmanned aerial vehicle comprises an unmanned aerial vehicle body, an undercarriage, wing rods, propellers, a capturing device and an intercepting device, wherein the unmanned aerial vehicle body is detachably connected with the undercarriage and is positioned above the undercarriage, a plurality of wing rods are uniformly arranged around the unmanned aerial vehicle body, the propellers are arranged at one end, far away from the unmanned aerial vehicle body, of each wing rod, the capturing device is arranged at the top of the unmanned aerial vehicle body, a storage cavity is arranged inside the unmanned aerial vehicle body, the intercepting device is arranged in the storage cavity, the capturing device comprises a mounting frame, a wireless radar, a compound eye camera and a high-frequency transmitter, the mounting frame is detachably connected with the unmanned aerial vehicle body and is positioned above the unmanned aerial vehicle body, the wireless radar, the compound eye camera and the high-frequency generator are arranged on the mounting frame, the intercepting device comprises an adjustable storage frame, a transmitting device and an intercepting net body, the adjustable storage frame is detachably connected with the unmanned aerial vehicle body and is located in the storage cavity, the adjustable storage frame is far away from one end of the unmanned aerial vehicle body, the transmitting device is arranged in the transmitting device, and the intercepting net body is arranged in the transmitting device.
2. The unmanned aerial vehicle intercepting apparatus of claim 1,
the adjustable storage rack comprises a connecting plate, a base, a rotating device, a rotating plate, an electric push rod, a placing plate, a turnover seat and a turnover device, the connecting plate is detachably connected with the unmanned aerial vehicle body, and is positioned in the containing cavity, the base is detachably connected with the connecting plate, one end of the base, which is far away from the connecting plate, is provided with a groove, the rotating device is arranged in the groove, the output end of the rotating device is provided with the rotating plate, the mounting end of the electric push rod is detachably connected with the rotating plate, the pushing end of the electric push rod is detachably connected with the placing plate, the placing plate is provided with a turnover frame and the turnover device, the turnover seat is movably connected with the turnover frame, the output end of the turnover device is matched with the turnover seat, and the emission device is arranged on the turnover seat.
3. The unmanned aerial vehicle intercepting apparatus of claim 2,
the rotating device comprises a first motor and a first reduction gearbox, the first motor is detachably connected with the base, the first reduction gearbox is arranged at the output end of the first motor, the rotating plate is arranged at the output end of the first reduction gearbox, a partition plate is arranged inside the base and located between the first motor and the first reduction gearbox, and the first reduction gearbox is detachably connected with the partition plate.
4. The unmanned aerial vehicle intercepting apparatus of claim 2,
the turnover device comprises a second motor, a second reduction gearbox, a rotating shaft and a clamping tooth, the second motor is detachably connected with the placing plate, the second reduction gearbox is arranged at the output end of the second motor, the rotating shaft is arranged at the output end of the second reduction gearbox, the clamping tooth is arranged at one end, away from the second reduction gearbox, of the rotating shaft, a clamping groove is formed in the turnover seat, and the clamping tooth is matched with the clamping groove.
5. The unmanned aerial vehicle intercepting apparatus of claim 1,
every the outside of screw all is provided with screw anticollision frame.
6. An unmanned aerial vehicle intercepting apparatus as defined in claim 5,
every screw anticollision frame all includes go-between, bracing piece and protection ring, the go-between cover is established the outside of wing pole, the protection ring cover is established the outside of screw, the outer wall of go-between with evenly be provided with many between the inner wall of protection ring the bracing piece, every the bracing piece all is the slope structure setting.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110281419.9A CN112977820A (en) | 2021-03-16 | 2021-03-16 | Unmanned aerial vehicle intercepting device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110281419.9A CN112977820A (en) | 2021-03-16 | 2021-03-16 | Unmanned aerial vehicle intercepting device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN112977820A true CN112977820A (en) | 2021-06-18 |
Family
ID=76335857
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202110281419.9A Pending CN112977820A (en) | 2021-03-16 | 2021-03-16 | Unmanned aerial vehicle intercepting device |
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| Country | Link |
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| CN (1) | CN112977820A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116022330A (en) * | 2021-10-25 | 2023-04-28 | 北京广监云科技有限公司 | Monitoring device for searching black broadcasting |
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|---|---|---|---|---|
| JP2016215874A (en) * | 2015-05-21 | 2016-12-22 | 株式会社熊谷組 | Capture device |
| US20170144756A1 (en) * | 2015-11-25 | 2017-05-25 | Mohammad Rastgaar Aagaah | Drone having drone-catching feature |
| CN207374645U (en) * | 2017-10-20 | 2018-05-18 | 施铠曼航空科技（上海）有限公司 | A kind of interception multi-rotor unmanned aerial vehicle |
| CN207482186U (en) * | 2017-11-03 | 2018-06-12 | 无锡莱特杰米科技发展有限公司 | A kind of quadrotor unmanned plane for training |
| EP3372499A1 (en) * | 2017-03-06 | 2018-09-12 | MBDA Deutschland GmbH | Unmanned aerial vehicle, system and method for countering flying threats |
-
2021
- 2021-03-16 CN CN202110281419.9A patent/CN112977820A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2016215874A (en) * | 2015-05-21 | 2016-12-22 | 株式会社熊谷組 | Capture device |
| US20170144756A1 (en) * | 2015-11-25 | 2017-05-25 | Mohammad Rastgaar Aagaah | Drone having drone-catching feature |
| EP3372499A1 (en) * | 2017-03-06 | 2018-09-12 | MBDA Deutschland GmbH | Unmanned aerial vehicle, system and method for countering flying threats |
| CN207374645U (en) * | 2017-10-20 | 2018-05-18 | 施铠曼航空科技（上海）有限公司 | A kind of interception multi-rotor unmanned aerial vehicle |
| CN207482186U (en) * | 2017-11-03 | 2018-06-12 | 无锡莱特杰米科技发展有限公司 | A kind of quadrotor unmanned plane for training |
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| CN116022330A (en) * | 2021-10-25 | 2023-04-28 | 北京广监云科技有限公司 | Monitoring device for searching black broadcasting |
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Application publication date: 20210618 |
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