CN113060283A - Pneumatic net gun device, unmanned aerial vehicle and pneumatic net gun launching system - Google Patents
Pneumatic net gun device, unmanned aerial vehicle and pneumatic net gun launching system Download PDFInfo
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- CN113060283A CN113060283A CN202110394991.6A CN202110394991A CN113060283A CN 113060283 A CN113060283 A CN 113060283A CN 202110394991 A CN202110394991 A CN 202110394991A CN 113060283 A CN113060283 A CN 113060283A
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- pneumatic net
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- net gun
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- 238000004891 communication Methods 0.000 claims description 16
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims description 12
- 230000005540 biological transmission Effects 0.000 claims description 9
- 238000009434 installation Methods 0.000 claims description 6
- 230000005484 gravity Effects 0.000 claims description 2
- 230000005611 electricity Effects 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 238000013459 approach Methods 0.000 description 2
- 230000006870 function Effects 0.000 description 2
- 238000003384 imaging method Methods 0.000 description 2
- 238000001931 thermography Methods 0.000 description 2
- 230000001960 triggered effect Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000005286 illumination Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 230000003595 spectral effect Effects 0.000 description 1
- 238000001228 spectrum Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Classifications
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- 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
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
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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
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
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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
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41B—WEAPONS FOR PROJECTING MISSILES WITHOUT USE OF EXPLOSIVE OR COMBUSTIBLE PROPELLANT CHARGE; WEAPONS NOT OTHERWISE PROVIDED FOR
- F41B15/00—Weapons not otherwise provided for, e.g. nunchakus, throwing knives
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- 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
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/34—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering
- H02J7/35—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering with light sensitive cells
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
Abstract
The invention relates to the technical field of pneumatic net guns, in particular to a pneumatic net gun device, an unmanned aerial vehicle and a pneumatic net gun launching system; including the nacelle platform, the inside first rotation motor that is provided with of nacelle platform, the output of first rotation motor runs through the nacelle platform and is connected with the pivot, the output of pivot is connected with supporting platform, supporting platform's bottom is equipped with the mounting bracket, it is connected with pneumatic net rifle main part to rotate on the mounting bracket, the side of mounting bracket is equipped with the second and rotates the motor, the output and the pneumatic net rifle main part of motor are connected to the second, pneumatic net rifle main part includes shell, three camera module, high-pressure air receiver and interception net. According to the invention, the pitching and azimuth movements can be realized by arranging the first rotating motor and the second rotating motor, the accurate control on the speed, the angle and the torque can be realized, the capturing hit rate is greatly improved, and the automatic triggering of the high-pressure air storage cylinder can be realized by arranging the triggering device.
Description
Technical Field
The invention relates to the technical field of pneumatic net guns, in particular to a pneumatic net gun device, an unmanned aerial vehicle and a pneumatic net gun launching system.
Background
The guidance unmanned aerial vehicle net throwing intercepting system is urban ultra-low altitude security equipment, applies a guidance technology to an unmanned aerial vehicle platform, realizes accurate guidance of a target, carries a pneumatic net gun, and implements soft killing interception on the target. The system adopts the GPS instruction guidance technology to approach the target remotely, the tail end adopts the vision guidance technology to control the unmanned aerial vehicle platform to approach the target with a proper posture, and finally the pneumatic net gun is triggered to carry out net throwing interception.
Therefore, a pneumatic net gun device, an unmanned aerial vehicle and a pneumatic net gun launching system are provided.
Disclosure of Invention
The invention aims to provide a pneumatic net gun device, an unmanned aerial vehicle and a pneumatic net gun launching system.
In order to achieve the purpose, the technical scheme of the invention is as follows:
a pneumatic net gun device comprises a pod platform, wherein a first rotating motor is arranged inside the pod platform, the output end of the first rotating motor penetrates through the pod platform and is connected with a rotating shaft, the output end of the rotating shaft is connected with a supporting platform, the first rotating motor is used for driving the supporting platform to rotate in the horizontal direction, a mounting frame is arranged at the bottom of the supporting platform, a pneumatic net gun main body is rotatably connected onto the mounting frame, a second rotating motor is arranged on the side face of the mounting frame, the output end of the second rotating motor is connected with the pneumatic net gun main body, the second rotating motor is used for driving the pneumatic net gun main body to rotate in the vertical direction, the pneumatic net gun main body comprises a shell, three camera modules, a high-pressure air storage cylinder and an intercepting net, the shell is of a hollow cylinder structure, and the rear end of the shell is provided with the high-pressure air, the front end of shell sets up the interception net, the output of high pressure gas receiver sets up towards the interception net, three camera module evenly sets up in the outside of shell along the geometric centre of gravity center of shell, be equipped with shift knob on the high pressure gas receiver, shift knob's top is equipped with trigger device, trigger device is used for triggering high pressure gas receiver work.
Specifically, trigger device includes linear electric motor and telescopic link, the high-pressure air receiver is put on the shelf and is equipped with the support, and the support sets up in shift knob's top, linear electric motor sets up on the support, the one end and the linear electric motor's of telescopic link output are connected, and the other end is connected with shift knob of high-pressure air receiver.
Specifically, a buffer spring is sleeved on the outer side of the telescopic rod.
Specifically, pneumatic net rifle main part still includes transmission head and a plurality of traction head, the transmission head sets up in the front end of shell, the interception net sets up inside the transmission head, the outward flange and the traction head of interception net are connected.
Specifically, the three camera modules are respectively an infrared thermal imager, an ultraviolet imager and a CCD camera.
The utility model provides an unmanned aerial vehicle, unmanned aerial vehicle includes fuselage, frame, four screws, flight control system and intelligent terminal, nacelle platform rigid coupling in the bottom of fuselage, the top of fuselage is provided with the installation cavity, be equipped with first storage battery, GPS orientation module and wireless communication module in the installation cavity, the top of fuselage is provided with the solar photovoltaic board, the solar photovoltaic board links to each other with first storage battery electricity, flight control system, GPS orientation module, three camera module are connected with intelligent terminal through wireless communication module respectively, flight control system, GPS orientation module, wireless communication module, three camera module, first rotation motor, second rotation motor, linear electric motor link to each other with first storage battery electricity respectively.
Specifically, the wireless communication module is one of 4G, 5G and ZigBee.
Specifically, the intelligent terminal is provided with a display screen, an operation key and a data transmission interface, and a storage module, a first processor and a second storage battery pack are arranged inside the intelligent terminal.
The utility model provides a pneumatic net rifle transmission system, pneumatic net rifle transmission system is the second controller, first rotation motor, second rotate motor, linear electric motor, wireless communication module are connected with the second controller electricity respectively, the second controller links to each other with first storage battery electricity.
The invention has the beneficial effects that: according to the invention, the pitching and azimuth movements can be realized by arranging the first rotating motor and the second rotating motor, the accurate control on the speed, the angle and the torque can be realized, the capturing hit rate is greatly improved, and the automatic triggering of the high-pressure air storage cylinder can be realized by arranging the triggering device.
Drawings
FIG. 1 is a schematic structural diagram of an embodiment of the present invention;
FIG. 2 is a schematic structural diagram of a pneumatic net gun body according to an embodiment of the invention;
fig. 3 is a schematic structural diagram of an intelligent terminal according to an embodiment of the present invention.
Reference numerals: the solar photovoltaic panel comprises a solar photovoltaic panel 1, a propeller 2, a machine body 3, a machine frame 4, a nacelle platform 5, a first rotating motor 6, a rotating shaft 7, a supporting platform 8, a second rotating motor 9, a mounting rack 10, an infrared thermal imager 11, an ultraviolet imager 12, a CCD camera 13, an intercepting net 14, an emitting head 15, a traction head 16, an intelligent terminal 17, a handle 18, an on-off key 19, a direction key 20, a high-pressure air storage cylinder 21, a switch button 22, a buffer spring 23, a shell 24, a support 25, a linear motor 26 and a display screen 27.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to the attached figure 2, the pneumatic net gun device comprises a pod platform 5, a first rotating motor 6 is arranged inside the pod platform 5, the output end of the first rotating motor 6 penetrates through the pod platform 5 to be connected with a rotating shaft 7, the output end of the rotating shaft 7 is connected with a supporting platform 8, the first rotating motor 6 is used for driving the supporting platform 8 to rotate in the horizontal direction, a mounting frame 10 is arranged at the bottom of the supporting platform 8, a pneumatic net gun main body is rotatably connected onto the mounting frame 10, a second rotating motor 9 is arranged on the side surface of the mounting frame 10, the output end of the second rotating motor 9 is connected with the pneumatic net gun main body, the second rotating motor 9 is used for driving the pneumatic net gun main body to rotate in the vertical direction, and the pneumatic net gun main body comprises a shell 24, three camera modules, a high-pressure air storage cylinder 21 and an intercepting net 14, the utility model discloses a high pressure gas receiver, including shell 24, high pressure gas receiver 21, three camera module, switch button 22, trigger device is equipped with trigger device, trigger device is used for triggering high pressure gas receiver 21 work, the rear end of shell 24 sets up high pressure gas receiver 21, the front end of shell 24 sets up interception net 14, high pressure gas receiver 21's output sets up towards interception net 14, three camera module evenly sets up in shell 24's the outside along shell 24's geometry focus center.
Furthermore, the first rotating motor 6 can drive the rotating shaft 7, the supporting platform 8 and the pneumatic net gun main body to rotate in the horizontal direction, so that the position of the pneumatic net gun main body in the horizontal direction can be adjusted, and meanwhile, the second rotating motor 9 can drive the pneumatic net gun main body to rotate in the vertical direction, namely the pitching angle of the pneumatic net gun main body is changed, so that the pneumatic net gun main body can work in all directions.
Specifically, the triggering device comprises a linear motor 26 and a telescopic rod, a support 25 is erected on the high-pressure air cylinder 21, the support 25 is arranged above the switch button 22, the linear motor 26 is arranged on the support 25, one end of the telescopic rod is connected with the output end of the linear motor 26, and the other end of the telescopic rod is connected with the switch button 22 of the high-pressure air cylinder 21; and a buffer spring 23 is sleeved outside the telescopic rod.
Further, the linear motor 26 according to the present invention can drive the telescopic rod to move in an extending and contracting manner, when the switch button 22 needs to be automatically triggered, the linear motor 26 drives the telescopic rod to move in an extending manner, and meanwhile, the linear motor is used in cooperation with the buffer spring 23, when the high pressure air cylinder 21 works, the recoil generated by the high pressure air cylinder 21 is reduced, and the service life of the linear motor 26 is prolonged.
Specifically, the pneumatic net gun main body further comprises a transmitting head 15 and a plurality of traction heads 16, the transmitting head 15 is arranged at the front end of the shell 24, the intercepting net 14 is arranged inside the transmitting head 15, and the outer edge of the intercepting net 14 is connected with the traction heads 16; by arranging the transmitting head 15 and the plurality of traction heads 16, after the intercepting net 14 is pushed to transmit by high-pressure gas sprayed from the high-pressure gas storage cylinder 21, the plurality of traction heads 16 move towards the direction of the axis far away from the shell 24.
Specifically, the three camera modules are an infrared thermal imager 11, an ultraviolet imager 12 and a CCD camera 13.
Further, the CCD camera 13 related to the invention adopts a Contax645AF camera, wherein the exposure time of the Contax645AF camera can reach 1/4000s at the fastest, and the CCD camera has small volume and complete functions.
Furthermore, the ultraviolet imager 12 provided by the invention adopts an SR27-SUPERB-QUANT ultraviolet imager 12, the wavelength of an ultraviolet channel is 240-280nm ultraviolet band, and a full-sun blind type ultraviolet imaging lens is provided, the lens collection area is 19cm2Under any sunlight intensity and weather conditions, the sunlight can be detected, the sunlight interference is avoided, and the imaging is clear.
Furthermore, the infrared thermal imager provided by the invention adopts an Altum type infrared thermal imager, wherein the Altum has five independent imagers which are respectively provided with a special optical filter, so that each imager can receive the spectrum in the wavelength range. The high-dynamic-range video camera is an industrial-grade imager, has high dynamic ranges in different illumination states, and does not have artifacts generated in video recording and photographing of a common unmanned aerial vehicle. Meanwhile, the system also has a thermal imaging function, and the standard 16-bit TIFF file output enables you to completely access the original data, so that you can process the system on a platform selected by you. The sensor can be used for splicing images of the sensor, processing data and the like, and providing index images such as NDVI, NDRE and the like. The output data can also be processed by software such as Pix 4D, NI, Photoscan and the like; five discontinuous spectral bands are collected simultaneously, 11um thermal imaging calibration is carried out, a repeatable measurement narrow-band filter provides large image resolution for a single band, image distortion on various platforms can be eliminated through a circular shutter design, the platform can operate alone, external triggering and data connection from an aircraft can be selected and connected with the aircraft through Ethernet or a serial port, direct configuration, state change and camera control are achieved, ground object resolution can reach 5.2 cm and be located at 120 m ground height, and a USB memory interface can provide 128GB storage.
Referring to attached drawings 1 and 3, an unmanned aerial vehicle comprises a body 3, a frame 4, four propellers 2, a flight control system and an intelligent terminal 17, a pod platform 5 is fixedly connected to the bottom of the body 3, an installation cavity is arranged at the top of the body 3, a first storage battery pack, a GPS positioning module and a wireless communication module are arranged in the installation cavity, a solar photovoltaic panel 1 is arranged at the top of the body 3, the solar photovoltaic panel 1 is electrically connected with the first storage battery pack, the flight control system, the GPS positioning module and the three camera modules are respectively connected with the intelligent terminal 17 through the wireless communication module, and the flight control system, the GPS positioning module, the wireless communication module, the three camera modules, the first rotating motor 6, the second rotating motor 9 and the linear motor 26 are respectively electrically connected with the first storage battery pack.
Further, a motor and an electric regulator are further arranged on the machine body 3, wherein the motor is a brushless motor and is used for mounting the propeller 2, the rotating speed of the motor is controlled through the electric regulator, and the motor and the electric regulator are respectively electrically connected with the first storage battery pack and the flight control system.
Furthermore, the flight control system provided by the invention is a flight control board.
Specifically, the wireless communication module is one of 4G, 5G and ZigBee.
Specifically, the intelligent terminal 17 is provided with a display screen 27, an operation key and a data transmission interface, and the intelligent terminal 17 is internally provided with a storage module, a first processor and a second storage battery.
Further, the intelligent terminal 17 related to the invention mainly comprises a machine body 3 driving system; the driving system of the unmanned aerial vehicle body 3 ensures that the unmanned aerial vehicle can stably fly; the first processor is connected with the second controller through the wireless communication module, and then the first rotating motor 6 and the second rotating motor 9 of real-time control carry out work, and then realize that three camera module gathers the image of formation of image target and obtains the positional information of target, after satisfying corresponding seizure and judging, the second controller drives linear electric motor 26 and carries out work, and linear electric motor 26 drives the telescopic link and extends the removal, accomplishes the transmission of pneumatic net rifle.
Further, the operation keys according to the present invention include an on-off key 19, a menu key, a switch key, a set key, a return key, a save key, a set key, and a direction key 20.
Further, handles 18 are further arranged on two sides of the intelligent terminal 17, and operation is facilitated.
A pneumatic net gun launching system is a second controller, a first rotating motor 6, a second rotating motor 9, a linear motor 26 and a wireless communication module are respectively and electrically connected with the second controller, and the second controller is electrically connected with a first storage battery pack.
Further, the solar photovoltaic panel 1 according to the present invention is used for providing electric energy for the first battery pack.
Finally, the above embodiments are only for illustrating the technical solutions of the present invention and not for limiting, although the present invention has been described in detail with reference to the preferred embodiments, it should be understood by those skilled in the art that modifications or equivalent substitutions may be made to the technical solutions of the present invention without departing from the spirit and scope of the technical solutions of the present invention, and all of them should be covered in the claims of the present invention.
Claims (9)
1. A pneumatic net gun device is characterized by comprising a pod platform, wherein a first rotating motor is arranged inside the pod platform, the output end of the first rotating motor penetrates through the pod platform to be connected with a rotating shaft, the output end of the rotating shaft is connected with a supporting platform, the first rotating motor is used for driving the supporting platform to rotate in the horizontal direction, a mounting frame is arranged at the bottom of the supporting platform, a pneumatic net gun main body is rotatably connected onto the mounting frame, a second rotating motor is arranged on the side surface of the mounting frame, the output end of the second rotating motor is connected with the pneumatic net gun main body, the second rotating motor is used for driving the pneumatic net gun main body to rotate in the vertical direction, the pneumatic net gun main body comprises a shell, three camera modules, a high-pressure air cylinder and an intercepting net, the shell is of a hollow cylindrical structure, and the rear end of the shell is provided with the high-pressure air cylinder, the front end of shell sets up the interception net, the output of high pressure gas receiver sets up towards the interception net, three camera module evenly sets up in the outside of shell along the geometric centre of gravity center of shell, be equipped with shift knob on the high pressure gas receiver, shift knob's top is equipped with trigger device, trigger device is used for triggering high pressure gas receiver work.
2. The pneumatic net gun device according to claim 1, wherein the triggering device comprises a linear motor and a telescopic rod, the high-pressure air cylinder is provided with a support on the upper frame, the support is arranged above the switch button, the linear motor is arranged on the support, one end of the telescopic rod is connected with the output end of the linear motor, and the other end of the telescopic rod is connected with the switch button of the high-pressure air cylinder.
3. The pneumatic net gun device according to claim 2, wherein a buffer spring is sleeved outside the telescopic rod.
4. The pneumatic net gun device according to claim 1, wherein the pneumatic net gun body further comprises a transmitting head and a plurality of drawing heads, the transmitting head is arranged at the front end of the shell, the intercepting net is arranged inside the transmitting head, and the outer edge of the intercepting net is connected with the drawing heads.
5. The pneumatic net gun device according to claim 1, wherein the three camera modules are an infrared thermal imager, an ultraviolet imager and a CCD camera.
6. An unmanned aerial vehicle comprising the pneumatic net gun apparatus of any one of claims 1-5, it is characterized in that the unmanned aerial vehicle comprises a body, a frame, four propellers, a flight control system and an intelligent terminal, the nacelle platform is fixedly connected to the bottom of the body, the top of the body is provided with an installation cavity, a first storage battery pack, a GPS positioning module and a wireless communication module are arranged in the installation cavity, the top of the machine body is provided with a solar photovoltaic panel which is electrically connected with a first storage battery pack, the flight control system, the GPS positioning module and the three camera modules are respectively connected with the intelligent terminal through the wireless communication module, the flight control system, the GPS positioning module, the wireless communication module, the three camera modules, the first rotating motor, the second rotating motor and the linear motor are electrically connected with the first storage battery respectively.
7. A drone according to claim 6, wherein the wireless communication module is one of 4G, 5G or ZigBee.
8. The unmanned aerial vehicle of claim 6, wherein the intelligent terminal is provided with a display screen, an operation key and a data transmission interface, and a storage module, a first processor and a second storage battery are arranged inside the intelligent terminal.
9. A pneumatic net gun launching system is characterized by comprising the pneumatic net gun device of any one of claims 1-5 and the unmanned aerial vehicle of any one of claims 6-8, wherein the pneumatic net gun launching system is a second controller, the first rotating motor, the second rotating motor, the linear motor and the wireless communication module are electrically connected with the second controller respectively, and the second controller is electrically connected with the first storage battery pack.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110394991.6A CN113060283A (en) | 2021-04-13 | 2021-04-13 | Pneumatic net gun device, unmanned aerial vehicle and pneumatic net gun launching system |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110394991.6A CN113060283A (en) | 2021-04-13 | 2021-04-13 | Pneumatic net gun device, unmanned aerial vehicle and pneumatic net gun launching system |
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| CN113060283A true CN113060283A (en) | 2021-07-02 |
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| CN202110394991.6A Pending CN113060283A (en) | 2021-04-13 | 2021-04-13 | Pneumatic net gun device, unmanned aerial vehicle and pneumatic net gun launching system |
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Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20170073070A1 (en) * | 2013-02-06 | 2017-03-16 | Zhou Tian Xing | Amphibious vertical takeoff and landing unmanned device with artificial intelligence (AI) and method and system for managing a crisis environment and controlling one or more targets |
| CN106995059A (en) * | 2017-03-20 | 2017-08-01 | 东华大学 | A kind of unmanned aerial vehicle onboard net gun apparatus |
| CN107193025A (en) * | 2017-07-14 | 2017-09-22 | 陕西舜洋电子科技有限公司 | A kind of orientable unmanned environment measuring station |
| CN108583889A (en) * | 2018-04-28 | 2018-09-28 | 北京机械设备研究所 | A kind of unmanned aerial vehicle onboard pneumatically throws net device |
| CN108700470A (en) * | 2015-12-09 | 2018-10-23 | 菲力尔系统公司 | Thermal imaging and paradigmatic system based on UAV system and method |
| CN109510971A (en) * | 2019-01-08 | 2019-03-22 | 中南林业科技大学 | A kind of wild animal intelligence observation system based on Internet of Things |
| CN110182363A (en) * | 2019-04-26 | 2019-08-30 | 厦门大学 | It is a kind of for capturing the flying wing type unmanned plane of unmanned plane |
| CN209521849U (en) * | 2018-12-10 | 2019-10-22 | 天津市宏宇天翔科技有限公司 | A kind of airship formula unmanned plane |
| CN209889115U (en) * | 2019-04-02 | 2020-01-03 | 广州鼎飞航空科技有限公司 | Unmanned aerial vehicle catches net device and unmanned aerial vehicle |
| CN112078796A (en) * | 2020-08-19 | 2020-12-15 | 北京机械设备研究所 | Pneumatic net gun device, unmanned aerial vehicle and pneumatic net gun launching system |
-
2021
- 2021-04-13 CN CN202110394991.6A patent/CN113060283A/en active Pending
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20170073070A1 (en) * | 2013-02-06 | 2017-03-16 | Zhou Tian Xing | Amphibious vertical takeoff and landing unmanned device with artificial intelligence (AI) and method and system for managing a crisis environment and controlling one or more targets |
| CN108700470A (en) * | 2015-12-09 | 2018-10-23 | 菲力尔系统公司 | Thermal imaging and paradigmatic system based on UAV system and method |
| CN106995059A (en) * | 2017-03-20 | 2017-08-01 | 东华大学 | A kind of unmanned aerial vehicle onboard net gun apparatus |
| CN107193025A (en) * | 2017-07-14 | 2017-09-22 | 陕西舜洋电子科技有限公司 | A kind of orientable unmanned environment measuring station |
| CN108583889A (en) * | 2018-04-28 | 2018-09-28 | 北京机械设备研究所 | A kind of unmanned aerial vehicle onboard pneumatically throws net device |
| CN209521849U (en) * | 2018-12-10 | 2019-10-22 | 天津市宏宇天翔科技有限公司 | A kind of airship formula unmanned plane |
| CN109510971A (en) * | 2019-01-08 | 2019-03-22 | 中南林业科技大学 | A kind of wild animal intelligence observation system based on Internet of Things |
| CN209889115U (en) * | 2019-04-02 | 2020-01-03 | 广州鼎飞航空科技有限公司 | Unmanned aerial vehicle catches net device and unmanned aerial vehicle |
| CN110182363A (en) * | 2019-04-26 | 2019-08-30 | 厦门大学 | It is a kind of for capturing the flying wing type unmanned plane of unmanned plane |
| CN112078796A (en) * | 2020-08-19 | 2020-12-15 | 北京机械设备研究所 | Pneumatic net gun device, unmanned aerial vehicle and pneumatic net gun launching system |
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Application publication date: 20210702 |