CN110030879A - A kind of unmanned aerial vehicle onboard platform catches net emitter - Google Patents
A kind of unmanned aerial vehicle onboard platform catches net emitter Download PDFInfo
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- CN110030879A CN110030879A CN201910447609.6A CN201910447609A CN110030879A CN 110030879 A CN110030879 A CN 110030879A CN 201910447609 A CN201910447609 A CN 201910447609A CN 110030879 A CN110030879 A CN 110030879A
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- 238000005183 dynamical system Methods 0.000 claims abstract description 16
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 12
- 229910052802 copper Inorganic materials 0.000 claims description 11
- 239000010949 copper Substances 0.000 claims description 11
- 230000008878 coupling Effects 0.000 claims description 11
- 238000010168 coupling process Methods 0.000 claims description 11
- 238000005859 coupling reaction Methods 0.000 claims description 11
- 238000009423 ventilation Methods 0.000 claims description 5
- 230000002035 prolonged effect Effects 0.000 claims 1
- 230000006378 damage Effects 0.000 abstract description 5
- 238000005516 engineering process Methods 0.000 abstract description 3
- 230000000694 effects Effects 0.000 description 9
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 8
- 238000010586 diagram Methods 0.000 description 6
- 229910002092 carbon dioxide Inorganic materials 0.000 description 4
- 238000010304 firing Methods 0.000 description 3
- 239000004677 Nylon Substances 0.000 description 2
- 240000007643 Phytolacca americana Species 0.000 description 2
- 208000002925 dental caries Diseases 0.000 description 2
- 238000002347 injection Methods 0.000 description 2
- 239000007924 injection Substances 0.000 description 2
- 229920001778 nylon Polymers 0.000 description 2
- 238000007789 sealing Methods 0.000 description 2
- 208000012260 Accidental injury Diseases 0.000 description 1
- 229920000742 Cotton Polymers 0.000 description 1
- 108091092878 Microsatellite Proteins 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
- 239000001569 carbon dioxide Substances 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 208000014674 injury Diseases 0.000 description 1
- 231100000518 lethal Toxicity 0.000 description 1
- 230000001665 lethal effect Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
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- 238000000034 method Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000006855 networking Effects 0.000 description 1
- 238000009527 percussion Methods 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
Classifications
-
- 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
- F41H11/04—Aerial barrages
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- General Engineering & Computer Science (AREA)
- Emergency Lowering Means (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Abstract
A kind of unmanned aerial vehicle onboard platform catches net emitter, is related to the aerial field of security technology of unmanned plane, including outer cover, net system of catching, pressure charging system, triggering system, dynamical system and launch control system are provided in outer cover；This is caught net emitter and realizes rotation Trigger Function, safety lock function, catches net emission function, pressurization ejecting function；This catches net emitter small volume, it can be mounted on most of unmanned aerial vehicle platform and use, it can implement soft destruction to flying objects such as black winged consumer level unmanned planes and capture control, it is light and handy flexible, it can be used for the defence and capture of low latitude unmanned plane soft destruction formula, provide technical support for public administrative departments and safety law enforcement department.
Description
Technical field
The present invention relates to the aerial field of security technologies of unmanned plane.
Background technique
With the rapid development in domestic and international unmanned plane market, the miniature drone product based on personal consumption end is increasingly
Mostly it is applied to different fields.While such " low slow small " aerial dynamic object is that consumer brings joyful experience, no
The safety of urban public utilities and place and the security privacy of residential block are influenced avoidablely, or even are become terrorist and used
To do the tool of the attack of terrorism.
There are low value, high accidental injury, weak protection, time is not true for defence " low slow small " aircraft in airport or urban environment
The features such as fixed and background image is complicated.Conventional equipment cannot adapt to these new features very well, and specific manifestation has: conventional missile is to anti-
It probably fights or city operation has the shortcomings that concealment is small, portability is poor, then high cost effectiveness is excessively high to miniature drone；Conventional bullet
Or then precision is insufficient for shell, not only success rate is low, but also has the shortcomings that easily accidentally injuring miss bomb；Laser Interception system is to " low slow small " mesh
Good effect is indicated, but there is also volumes simultaneously disadvantage big, inconvenient to carry or hiding.
Summary of the invention
For the problems in the relevant technologies, the purpose of the present invention is to propose to it is a kind of it is light and handy flexibly, opened using rotary triggering
It closes, can be used for the unmanned aerial vehicle onboard platform of defence and the capture of low latitude unmanned plane soft destruction formula catches net emitter.
The present invention includes outer cover, be provided in the outer cover net system of catching, pressure charging system, triggering system, dynamical system and
Launch control system；It is described catch net system for load catch net and drive catch net injection；The pressure charging system is set to and catches net system
Between triggering system, auxiliary power is provided to catch net system for increasing gas pressure intensity；The triggering system is dynamic for triggering
Force system；The dynamical system is for loading gas cylinder；The launch control system is for receiving transmitting signal and driving dynamical system
The net of catching that opposite triggering system of uniting works to make to catch net system projects.
Further, the launch control system includes motor and the shaft coupling that connect with motor output shaft, the electricity
Machine is mounted on motor fixing plate, and the motor fixing plate is fixedly connected by screw with outer cover.
Further, the dynamical system includes power plant module, the compressed gas cylinder in power plant module, the power mould
The bottom of block is equipped with a bottom plug, and the shaft coupling of the bottom plug and launch control system connects, in the upper end of the power plant module
Wall is equipped with a sliding slot being obliquely installed, and the upper end of the power plant module is additionally provided with two air channels, and the power plant module
Upper end extends in triggering system.
Further, the triggering system includes the trigger module being screwed on power plant module, hitting in trigger module
Needle and pressure spring, the pressure spring are set to the top of striker, and the side of the pressure spring is equipped with button, and the button is equipped with button bullet
Spring, the tip of the striker and the bottleneck of compressed gas cylinder are correspondingly arranged, and the striker is equipped with a bayonet lock；The trigger module
Inner wall and power plant module outer wall upper end between form a gas circuit cavity, the gas circuit cavity is communicated with two air channels.
Further, the top of the pressure spring is equipped with one for fixing the fixing lug boss of pressure spring, the fixing lug boss it is upper
Side is equipped with support platform, and the support platform is equipped with several first ventholes, the gas circuit cavity and several are first logical
Stomata communicates.
Further, the net system of catching includes catching net module, and the net module of catching includes revolving with trigger module upper end
The first boss and second boss connect, the first boss is interior to be equipped with a hollow cavity, and the lower end of the hollow cavity extends
To support platform, the upper end of the hollow cavity extends to second boss；The top of the second boss is equipped with a cone tank,
Net packet is equipped in the cone tank, the outer wall of the cone tank is equipped with six third ventholes being annularly obliquely installed.
Further, six third ventholes are extended to the cone bottom of cone tank outer wall by the vertex of a cone of cone tank outer wall,
And the bottom of each third venthole is correspondingly arranged and communicates with the second venthole in second boss, each third
The top of venthole is equipped with a tapered weight block, and the weight block is connect with the hexagonal of net packet.
Further, the pressure charging system includes boost module, and the boost module is a scale copper, and the scale copper is set
Between hollow cavity and second boss.
Further, the top of the weight block is equipped with a baffle, and the baffle is fixed by end cap.
The present invention realizes rotation using net system, pressure charging system, triggering system, dynamical system and launch control system is caught
Turn Trigger Function, safety lock function, catch net emission function, pressurization ejecting function；This catches net emitter small volume, can carry
It is used on most of unmanned aerial vehicle platform, soft destruction can be implemented to flying objects such as black winged consumer level unmanned planes and captured
Control, it is light and handy flexibly to can be used for the defence and capture of low latitude unmanned plane soft destruction formula, it is public administrative departments and safety law enforcement portion
Door provides technical support.
Detailed description of the invention
Fig. 1 is overall structure diagram of the invention.
Fig. 2 is the structural schematic diagram of power plant module in the present invention.
The sectional view along A-A of Fig. 3 Fig. 2.
Fig. 4 is the structural schematic diagram of trigger module in the present invention.
Fig. 5 is the B-B direction cross-sectional view of Fig. 3.
Fig. 6 is the structural schematic diagram that net module is caught in the present invention.
Fig. 7 is the structural schematic diagram of striker in the present invention.
Fig. 8 is the structural schematic diagram of weight block in the present invention.
In figure: 1 outer cover, 2 motors, 3 shaft couplings, 4 motor fixing plates, 5 screws, 6 power plant modules, 6-1 sliding slot, 6-2 ventilation
Slot, 7 compressed gas cylinders, 8 bottom plugs, 9 trigger modules, 10 strikers, the tip 10-1,11 pressure springs, 12 buttons, 13 button springs, 14 bayonet locks,
Net module, 19 first boss, 20 second are caught in 15 gas circuit cavitys, 16 fixing lug boss, 17 support platforms, the first venthole of 17-1,18
Boss, the second venthole of 20-1,21 hollow cavities, 22 cone tanks, 23 net packets, 24 third ventholes, 25 weight blocks, 26 thin copper
Piece, 27 baffles, 28 end caps.
Specific embodiment
As shown in figures 1-8, net system of catching, pressurization are provided in the outer cover 1 for catching net emitter of unmanned aerial vehicle onboard platform
System, triggering system, dynamical system and launch control system；Catch net system for load catch net and drive catch net injection；Pressurization
System is set to and catches between net system and triggering system, provides auxiliary power for increasing gas pressure intensity to catch net system；Triggering system
System is for triggering dynamical system；Dynamical system is for loading gas cylinder；Launch control system is for receiving transmitting signal and driving dynamic
Force system is projected with respect to the net of catching that triggering system works to make to catch net system.
In the present embodiment, using net system, pressure charging system, triggering system, dynamical system and launch control system is caught, realize
Rotation Trigger Function, safety lock function catch net emission function, pressurization ejecting function；Meanwhile this catch net emitter volume compared with
It is small, it can be mounted on most of unmanned aerial vehicle platform and use, the flying objects such as black winged consumer level unmanned plane can be implemented soft
Lethal capture control.Wherein, the effect of outer cover it is main there are three: the first, outer cover is mainly used to be isolated inner body and external
Environment, to achieve the effect that protect inner body；The second, outer cover is used to block the button on trigger module, prevents button from existing
It is launched away when device inflation percussion；Third, outer cover are used to the motor in fixed transmission control system: will by screw
Motor fixing plate is fixed, and motor fixing plate is fixed further through screw with motor, therefore motor will be consolidated relatively with outer cover
It is fixed.
Specifically, launch control system includes motor 2 and exports the shaft coupling 3 of axis connection with motor 2, motor 2 is installed
On motor fixing plate 4, motor fixing plate 4 is fixedly connected by screw 5 with outer cover 1.
In the present embodiment, catching net firing order can be connected in the form of electric current on motor 2, and energization motor 2 rotates, from
And drive shaft coupling 3 to rotate, and then drive bottom plug rotation, it can thus drive power plant module to rotate relative to trigger module, thus
Net emission switch is caught in triggering, will be caught net and is projected.It is worth noting that the connection screw thread rotation direction of bottom plug and power plant module should be with power
The thread rotary orientation that module is connected with trigger module is opposite.And the rotation direction of motor 2 should be with the rotation of power plant module and bottom plug connection screw thread
To identical, just being can guarantee when motor 2 starts in this way is power plant module relative to trigger module rotation rather than bottom plug is opposite
It is rotated in power plant module.Wherein, for motor 2 using the small machine of model 395, shaft coupling 3 uses box coupling, and uses spiral shell
Bolt is tightened.
Specifically, dynamical system includes power plant module 6, the compressed gas cylinder 7 in power plant module 6, the bottom of power plant module 6
Portion is equipped with a bottom plug 8, and bottom plug 8 is connect with the shaft coupling 3 of launch control system, and the upper end inner wall of power plant module 6 is equipped with one and inclines
The sliding slot 6-1 being tiltedly arranged, the upper end of power plant module 6 is additionally provided with two air channel 6-2, and the upper end of power plant module 6 extends
Into triggering system.
In the present embodiment, compressed gas cylinder 7 uses CO2 specification for the compressed gas cylinder of 12g, the main body of the effect of power plant module 6
Now both ways: on the one hand be load compressed gas cylinder 7, on the other hand with it is rotary in trigger module group networking packet flick mechanism
Trigger switch；In addition the lower part of power plant module 6 is also connected with motor with the launch control system that shaft coupling is constituted, and power plant module
The bottom of 6 inner cavities uses with bottom plug 8 and is threadedly coupled；Using the effect for the sliding slot 6-1 being obliquely installed, following strikers is enable to slide
Enter triggering compressed gas cylinder 7 in the sliding slot 6-1 of power plant module 6, and slowly bullet playbacks under the action of following pressure springs；Two air channels
6-2 is both designed as kidney-shaped shape, in this way for increasing outlet area.
Specifically, triggering system includes the trigger module 9 being screwed on power plant module 6, the striker 10 in trigger module 9
With pressure spring 11, pressure spring 11 is set to the top of striker 10, and the side of pressure spring 11 is equipped with button 12, and button 12 is equipped with button spring
13, the tip 10-1 and the bottleneck of compressed gas cylinder 7 of striker 10 are correspondingly arranged, and striker 10 is equipped with a bayonet lock 14；Trigger module 9
6 outer wall of inner wall and power plant module upper end between form a gas circuit cavity 15, gas circuit cavity 15 and two air channel 6-2 phases
It is logical.
Wherein, the top of pressure spring 11 is equipped with one for fixing the fixing lug boss 16 of pressure spring 11, and the top of fixing lug boss 16 is set
There is support platform 17, support platform 17 is equipped with several first ventholes 17-1, gas circuit cavity 15 and several first ventilations
Hole 17-1 is communicated.
In the present embodiment, the main effect of the trigger module 9 is: the spring and striker for firing compressed gas cylinder are loaded,
The compressed gas of guidance gas cylinder release rushes at scale copper and catches net module, accepts catch net module upwards, connect power mould downwards
Block.Button 12 is similar to the mechanism of pistol insurance class, to prevent triggering the present apparatus during transport or storage；Pressure spring 11 is used for
The sealing of striker impact compressed gas cylinder is pushed, compressed gas cylinder discharges gas；The effect of bayonet lock 14 are as follows: guarantee when the cunning on power plant module
The top of power plant module can withstand striker when slot is not overlapped with the bayonet lock in the striker on trigger module, and when sliding slot and bayonet lock weight
Bayonet lock can smoothly enter into power plant module and poke the sealing of gas cylinder to release compressed CO2 gas when conjunction, and CO2 gas is logical
It crosses in two air channel 6-2 guiding gas circuit cavitys 15；When practical application, in fixing lug boss 16 also should aperture, avoided gas
It cannot circulate away after into the region where pressure spring.Wherein, tip 10-1 is used to poke the bottleneck of compressed gas cylinder 7.
Specifically, catching net system includes catching net module 18, catching net module 18 includes the to be screwed on 9 upper end of trigger module
One boss 19 and second boss 20, first boss 19 is interior to be equipped with a hollow cavity 21, and the lower end of hollow cavity 21 extends to branch
Platform 17 is supportted, the upper end of hollow cavity 21 extends to second boss 20；The top of second boss 20 is equipped with a cone tank 22, cone
Net packet 23 is equipped in shape slot 22, the outer wall of cone tank 22 is equipped with six third ventholes 24 being annularly obliquely installed.
Wherein, six third ventholes 24 are extended to the cone bottom of 22 outer wall of cone tank by the vertex of a cone of 22 outer wall of cone tank, and
The bottom of each third venthole 24 is correspondingly arranged and communicates with the second venthole 20-1 in second boss 20, and each third is logical
The top of stomata 24 is equipped with a tapered weight block 25, and weight block 25 is connect with the hexagonal of net packet 23.
In the present embodiment, above-mentioned compressed gas cylinder, power plant module, striker, pressure spring, trigger module constitute the net packet bullet of the present apparatus
Opening mechanism, main function are as follows: compressed gas projects weight block along six third ventholes 24, so that net packet 23 be driven to penetrate
Out.Wherein, the outer wall of first boss 19 is equipped with screw thread, convenient for catch net module 18 and be screwed on, the second ventilation in second boss 20
It there are six hole 20-1 is set, and is arranged in a one-to-one correspondence in six third ventholes 24, and six 24 uniform intervals of third venthole are set
It sets, prevents gas pressure is excessively high from duct being caused to burst phenomenon.In actual design, the diameter of third venthole 24 is 4mm, six
The inscribed diameter of a circle of the hexagon of the center of circle composition of second venthole 20-1 is 8mm, and 21 diameter of hollow cavity is 14mm, this
Sample, which can meet, makes the stronger requirement of gas pressure in duct.Six equal solid constructions of weight block 25, are individually positioned in six thirds
In venthole 24, weight block 25 can block the port of third venthole 24 under the effect of gravity, to guarantee that its is airtight
Property, and the connecting hole for connecting with net packet 23 is equipped in the tail end of weight block 25.Net packet 23 is regular hexagon net, and when expansion is interior
Connecing circular diameter is 2 meters, and mesh is dimensioned to 3 centimetres, and the main material of cable has: cotton thread, PA nylon wire, PE line；This reality
Apply the preferred PA nylon wire of example.
Specifically, pressure charging system includes boost module, boost module is a scale copper 26, and scale copper 26 is set to hollow cavity
Between 21 and second boss 20.
In the present embodiment, the effect of the scale copper 26 are as follows: in order to avoid not strong enough towards the gas pressure for catching net module
The range of net is caught in influence, can be blocked by scale copper 26 when compressed gas is altered up from below, until gas pressure intensity arrives greatly punching
It has broken scale copper 26 and could up reach and caught net module to firing weight block.
Specifically, the top of weight block 25 is equipped with a baffle 27, baffle 27 is fixed by end cap 28.
In the present embodiment, baffle 27 is for blocking net packet and weight block, being on the one hand to prevent from laying flat in this way or falling
Net packet and weight block are fallen when putting device；On the other hand it is slightly to stop weight block, increases weight block and launch away
When gas pressure, the range for making to catch net increases by one point.End cap 28 is used for fixed baffle 27, set on the most upper of whole device
End, is connected through a screw thread with net module is caught.
The working principle of the invention: after the device receives transmitting signal, motor drives compressed gas cylinder to rotate relative to striker, rotation
Striker rushes open compressed gas cylinder after going to suitable position, and gas cylinder discharges compressed gas, and compressed gas is along the device gas set
Weight block is projected in path, projects to drive and catch net.Meanwhile the unmanned aerial vehicle onboard catches net emitter overall length 303mm, diameter
It for 40mm, uses 12 grams of carbon dioxide compression gas cylinders that will catch net as power and projects, 10 meters of range or so, catch the whole exhibitions of net
It is 2 meters of diameter of hexagon net when opening, the various flying objects of diameter 3cm or more can be captured；And originally catch net emitter can
Carry is on most of Small and micro-satellite platform.
In addition, need to only open outer cover and bottom cover when the device use, spring is pressed, gas cylinder is put into, covers bottom cover, is beaten
Insurance is opened, outer cover is installed, carry can be used on unmanned plane；Without using when compressed gas cylinder can be taken out and avoid accidentally touching
It sends out and causes the accident.
When practical application, the present apparatus can also install corresponding aiming module, communication module etc., its further reliability and standard additional
True property.
In addition, it is necessary to illustrate, compressed gas cylinder involved in the present embodiment, motor are the production bought on existing market
Product, therefore its structure and working principle etc. no longer elaborate herein.
Claims (9)
1. a kind of unmanned aerial vehicle onboard platform catches net emitter, including outer cover (1), which is characterized in that set in the outer cover (1)
It is equipped with net system of catching, pressure charging system, triggering system, dynamical system and launch control system；It is described catch net system for load catch
Net and drive are caught net and are projected；The pressure charging system is set to and catches between net system and triggering system, is to catch for increasing gas pressure intensity
Net system provides auxiliary power；The triggering system is for triggering dynamical system；The dynamical system is for loading gas cylinder；It is described
Launch control system is for receiving transmitting signal and dynamical system being driven to work to make to catch catching for net system with respect to triggering system
Net projects.
2. unmanned aerial vehicle onboard platform according to claim 1 catches net emitter, which is characterized in that the emission control
System includes that motor (2) and the shaft coupling (3) with motor (2) output axis connection, the motor (2) are mounted on motor and fix
On plate (4), the motor fixing plate (4) is fixedly connected by screw (5) with outer cover (1).
3. unmanned aerial vehicle onboard platform according to claim 2 catches net emitter, which is characterized in that the dynamical system
Including power plant module (6), the compressed gas cylinder (7) being set in power plant module (6), the bottom of the power plant module (6) is equipped with a bottom
It fills in (8), the bottom plug (8) connect with the shaft coupling (3) of launch control system, and the upper end inner wall of the power plant module (6) is set
There is a sliding slot (6-1) being obliquely installed, the upper end of the power plant module (6) is additionally provided with two air channels (6-2), and described dynamic
The upper end of power module (6) extends in triggering system.
4. unmanned aerial vehicle onboard platform according to claim 3 catches net emitter, which is characterized in that the triggering system
It is described including the trigger module (9) being screwed on power plant module (6), the striker (10) and pressure spring (11) that are set in trigger module (9)
Pressure spring (11) is set to the top of striker (10), and the side of the pressure spring (11) is equipped with button (12), and sets on the button (12)
Have button spring (13), the tip (10-1) of the striker (10) and the bottleneck of compressed gas cylinder (7) are correspondingly arranged, and the striker
(10) bayonet lock (14) are equipped with；One is formed between the inner wall of the trigger module (9) and the upper end of power plant module (6) outer wall
Gas circuit cavity (15), the gas circuit cavity (15) communicate with two air channels (6-2).
5. a kind of unmanned aerial vehicle onboard platform according to claim 4 catches net emitter, which is characterized in that the pressure spring
(11) top is equipped with one for fixing the fixing lug boss (16) of pressure spring (11), and the top of the fixing lug boss (16) is equipped with support
Platform (17), the support platform (17) be equipped with several first ventholes (17-1), the gas circuit cavity (15) with it is several
A first venthole (17-1) communicates.
6. unmanned aerial vehicle onboard platform according to claim 5 catches net emitter, which is characterized in that described to catch net system
Including catching net module (18), it is described catch net module (18) include the first boss (19) being screwed on trigger module (9) upper end and
Second boss (20), the first boss (19) is interior to be equipped with a hollow cavity (21), and the lower end of the hollow cavity (21) is prolonged
It extends to support platform (17), the upper end of the hollow cavity (21) extends to second boss (20)；The second boss (20)
Top be equipped with a cone tank (22), net packet (23) is equipped in the cone tank (22), the outer wall of the cone tank (22) is equipped with
Six third ventholes (24) being annularly obliquely installed.
7. unmanned aerial vehicle onboard platform according to claim 6 catches net emitter, which is characterized in that six thirds
Venthole (24) is extended to the cone bottom of cone tank (22) outer wall, and each third ventilation by the vertex of a cone of cone tank (22) outer wall
The bottom in hole (24) is correspondingly arranged and communicates with the second venthole (20-1) on second boss (20), each third ventilation
The top in hole (24) is equipped with a tapered weight block (25), and the weight block (25) connect with the hexagonal of net packet (23).
8. unmanned aerial vehicle onboard platform according to claim 6 catches net emitter, which is characterized in that the pressure charging system
Including boost module, the boost module is a scale copper (26), and the scale copper (26) is set to hollow cavity (21) and second
Between boss (20).
9. unmanned aerial vehicle onboard platform according to claim 7 catches net emitter, which is characterized in that the weight block
(25) top is equipped with a baffle (27), and the baffle (27) is fixed by end cap (28).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910447609.6A CN110030879B (en) | 2019-05-27 | 2019-05-27 | Net capturing and transmitting device of unmanned aerial vehicle carrying platform |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910447609.6A CN110030879B (en) | 2019-05-27 | 2019-05-27 | Net capturing and transmitting device of unmanned aerial vehicle carrying platform |
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| CN110030879A true CN110030879A (en) | 2019-07-19 |
| CN110030879B CN110030879B (en) | 2024-03-29 |
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| CN201910447609.6A Active CN110030879B (en) | 2019-05-27 | 2019-05-27 | Net capturing and transmitting device of unmanned aerial vehicle carrying platform |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110329530A (en) * | 2019-07-22 | 2019-10-15 | 黑龙江大学 | A kind of aerial low-speed unmanned aerial vehicle recyclable device of ejection net catching type |
| CN111959782A (en) * | 2020-08-27 | 2020-11-20 | 哈瓦国际航空技术（深圳）有限公司 | Unmanned plane |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201212795Y (en) * | 2008-04-08 | 2009-03-25 | 宋友江 | Air actuated capture net |
| JP3203272U (en) * | 2015-12-18 | 2016-03-24 | 株式会社ジェイウィン | Restraint screen projection device |
| CN107976118B (en) * | 2017-12-05 | 2020-02-07 | 江西鉴真防务技术有限公司 | Anti-unmanned aerial vehicle's seizure system |
| CN207716957U (en) * | 2018-01-17 | 2018-08-10 | 辽宁睿德航空科技有限公司 | A kind of police unmanned plane net rifle arrests module |
| CN109443097A (en) * | 2018-11-16 | 2019-03-08 | 南京理工大学 | A kind of acquisition equipment and catching method for rotor wing unmanned aerial vehicle |
| CN109579620A (en) * | 2018-12-06 | 2019-04-05 | 内蒙动力机械研究所 | A kind of unmanned plane flexibility capture systems and application method |
| CN210220837U (en) * | 2019-05-27 | 2020-03-31 | 江苏九设机器人科技有限公司 | Net catching and launching device of unmanned aerial vehicle airborne platform |
-
2019
- 2019-05-27 CN CN201910447609.6A patent/CN110030879B/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110329530A (en) * | 2019-07-22 | 2019-10-15 | 黑龙江大学 | A kind of aerial low-speed unmanned aerial vehicle recyclable device of ejection net catching type |
| CN110329530B (en) * | 2019-07-22 | 2020-06-05 | 黑龙江大学 | Ejection net capture type aerial medium-low speed unmanned aerial vehicle recovery device |
| CN111959782A (en) * | 2020-08-27 | 2020-11-20 | 哈瓦国际航空技术（深圳）有限公司 | Unmanned plane |
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| CN110030879B (en) | 2024-03-29 |
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