CN207540428U - A kind of unmanned plane blocking apparatus - Google Patents
A kind of unmanned plane blocking apparatus Download PDFInfo
- Publication number
- CN207540428U CN207540428U CN201721570195.9U CN201721570195U CN207540428U CN 207540428 U CN207540428 U CN 207540428U CN 201721570195 U CN201721570195 U CN 201721570195U CN 207540428 U CN207540428 U CN 207540428U
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- China
- Prior art keywords
- unmanned plane
- rocket launching
- elevation angle
- blocking apparatus
- bullet
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Abstract
The utility model discloses a kind of unmanned plane blocking apparatus, including transmitting stent, intercept net and multiple rocket launching bullets, wherein, the transmitting stent is equipped with the fixed seat identical with rocket launching bullet quantity, a rocket launching bullet is placed in each fixed seat, the multiple rocket launching bullet is connected to the edge of intercept net；The rocket launching bullet includes body, propeller, the radome fairing for being arranged on propeller upper end, the parachute being located in radome fairing, the parachute catapult-launching gear being located in radome fairing and the omniselector being located on rectification cover outer wall.The device can complete the interception task of unmanned plane harmlessly, and any device feature that will not fall during interception, it can be ensured that the people on ground and other properties not damaged.
Description
Technical field
The utility model is related to a kind of intercepting systems, and in particular to a kind of unmanned plane blocking apparatus.
Background technology
Recent year unmanned plane application development is swift and violent, unmanned plane agricultural, survey and draw, the fields such as take photo by plane have obtained widely
Using China gradually develops into World UAV center.Promotion and domestic unmanned plane prison with unmanned plane quantity
Tube body system it is not perfect.The black event for flying, disorderly flying of unmanned plane takes place frequently.Life and property safety to general public cause seriously
Threat.What is more, safety of civil aviation accident caused by some unmanned plane during flying events, caused by property loss it is huge.
International situation is intricate in recent years, illegal acquisition and spy for China's military information and geographical national conditions information
Activity takes place frequently, external most to carry out the illegal means such as take photo by plane using unmanned plane China's information is stolen, to the country in China
Safety constitutes a serious threat, therefore is badly in need of developing a simple and practical unmanned plane blocking apparatus, safeguards national information safety.
Authorization Notice No. is that " the anti-UAV Intelligent of net bullet formula intercepts disclosed in the application for a patent for invention of 105711850 A of CN
In system ", the unmanned plane attacked by detection early warning system discovery receives radar signal by control emission system and sends out interception
Instruction, arrests target by emitting intelligent intercept net bullet.Above-mentioned " the anti-UAV Intelligent intercepting system of net bullet formula " can
Unmanned plane is intercepted, but still is had the following problems：
1st, the intelligent intercept net bullet that the control emission system of the anti-UAV Intelligent intercepting system of above-mentioned net bullet formula projects is in bullet
Go out after unmanned plane wraps and collapsed by netting gear, it will fall, unmanned plane is damaged；
2nd, the net cylinder of intelligent intercept net bullet and net play it is fire-retardant cover on pop-up netting gear after come off, the two can to the people on ground and
The safety of other properties threatens.
Utility model content
The purpose of the utility model is to overcome the deficiencies and shortcoming of original technology, provide a kind of safer unmanned plane and block
Device is cut, it is harmless by unmanned plane Security distillation to achieve the purpose that, and any device feature that will not fall during interception,
It can ensure that and the people on ground and other properties are not damaged.
The utility model aim is achieved through the following technical solutions：
A kind of unmanned plane blocking apparatus, including transmitting stent, intercept net and multiple rocket launching bullets, wherein, the hair
It penetrates stent and is equipped with the fixed seat identical with rocket launching bullet quantity, a rocket launching bullet is placed in each fixed seat, it is described
Multiple rocket launching bullets are connected to the edge of intercept net；The rocket launching bullet includes body, propeller, is arranged on and pushes away
It radome fairing into device upper end, the parachute being located in radome fairing, the parachute catapult-launching gear being located in radome fairing and is located at whole
Flow the omniselector on cover outer wall.
One preferred embodiment of the utility model, wherein, the parachute catapult-launching gear is located at the lower section of parachute, including
The pulling assembly of centrally disposed compressed spring and setting circumferentially, wherein, the lower end of the compressed spring is fixed on bullet
On body, the upper end of compressed spring withstands on parachute bottom and in compressive state；The pulling assembly includes electromagnet and draw ring,
One end of draw ring is connect with parachute, and the ring body of the other end of draw ring is sleeved on the telescopic shaft of electromagnet.Under normality, parachute quilt
Be fixed in radome fairing, the effect of the downward pulling force of the telescopic shaft and draw ring of the upward elastic force of compressed spring and electromagnet and
In force balance state；When parachute needs are launched, electromagnet is powered, telescopic shaft make stretching motion and with the ring of draw ring
Body detaches, and the parachute after separation is gone out under the action of compressed spring elastic force by ejection.
Preferably, the radome fairing is put together by two and half radome fairings of left and right, passes through bolt between two and half radome fairings
It connects, automatic apparatus to cause bursting is equipped with the corresponding position of bolt on radome fairing.During the motion, when radome fairing needs and bullet
When body detaches, bolt disconnection unlocks radome fairing by automatic apparatus to cause bursting by igniting automatically, two and half radome fairings after unlock
Automatically it moves out and is detached from body, so as to fulfill the separation of radome fairing.
Preferably, the transmitting stent is equipped with support plate, is connected between the fixed seat and support plate by connecting rod,
The intercept net is supporting in support plate.By set the support plate can realize support to fixed seat and intercept net and
It is fixed.
Preferably, be equipped with universal ball end between the support plate and transmitting stent, wherein, rotor in universal ball end with
The support plate connection.By setting the universal ball end, fixed seat, connecting rod, intercept net and rocket launching are enabled to
Bullet integrally carries out the rotation of any direction, so as to fulfill the adjusting of whole elevation angle posture, is intercepted to emit to specific direction
Net.
Preferably, the connecting rod is electric telescopic rod.It, can by the stretching motion for controlling electric telescopic rod during work
The distance between rocket launching bullet is adjusted, so that rocket launching bullet can adapt to different size of intercept net, is realized to not
Unmanned plane with size is intercepted.The electric telescopic rod can have control system control, thus according to the size of intercept net,
The length of the adjusting connecting rod of adaptability.
Preferably, it is additionally provided with to snap into rocket launching row elevation angle attitude regulation between the connecting rod and transmitting stent
Elevation angle adjusting rod, which is made of electric telescopic rod, wherein, one end of elevation angle adjusting rod and support plate or connect
It is rotatablely connected between bar, is rotatablely connected between the other end and transmitting stent.During work, the motor in electric telescopic rod drives flexible
Bar makees stretching motion, so as to support plate, fixed seat, connecting rod, intercept net and rocket launching bullet are integrally pulled down or on
It pushes away to change its whole elevation angle posture；The electric telescopic rod can be controlled by control system, so as to according to quilt
It intercepts the orientation of unmanned plane and automatically regulates the direction of the launch and posture of intercept net, can more accurately and efficiently realize to nothing
Man-machine interception.
Preferably, the rocket launching bullet is four, and the elevation angle adjusting rod is four, every elevation angle adjusting rod and rocket
It is arranged in a one-to-one correspondence between transmitting bullet.It during work, cooperates between four elevation angle adjusting rods, such as an elevation angle adjusting rod is made
Upper push is moved, and three elevation angle adjusting rods make drop-down movement, and two elevation angle upper push of adjusting rods work for another example are moved, two elevation angle adjusting rods
Make drop-down movement, so as to integrally make the adjustment of the elevation angle posture of any direction to rocket launching bullet.
Preferably, it is additionally provided with to drive support plate, connecting rod, intercept net, fixed seat and fire on the transmitting stent
The rotary drive mechanism that is integrally rotated of arrow transmitting bullet, the rotary drive mechanism include the turntable being arranged on transmitting stent with
And the motor of driving disc rotation, wherein, the elevation angle adjusting rod is rotatably connected on turntable.During work, when turntable rotates band
During dynamic elevation angle adjusting rod rotation, since support plate, connecting rod, intercept net, fixed seat and rocket launching bullet are entirely through universal
Bulb is connect, therefore the entirety can rotate simultaneously with transmitting stent, in this way, carrying out multiple rocket launching bullet entirety posture tune
It during section, first passes through rotary drive mechanism and the circle distribution position of multiple rocket launching bullets is adjusted, then recycle one
Whole elevation angle posture is adjusted in elevation angle adjusting rod, so as to complete rocket launching bullet any circumference distribution and arbitrary
The dual regulation of elevation angle posture, therefore regulating effect is good.The motor can be controlled by control system, so as to automatically adjust
Save posture.
The operation principle of the unmanned plane blocking apparatus of the utility model is：
During work, which cooperates with early warning system, control system, common to complete blocking for unmanned plane
The task of cutting.Specifically, after unmanned plane flies into blank pipe no-fly zone, early warning system will detect and track the position of the unmanned plane of invasion
Confidence ceases, and communicates information to control system；The control system is believed according to the unmanned plane position that early warning system sends over
Breath controls the propeller igniting in intercepting system to start, and multiple rocket launching bullets can drive intercept net to go up to the air, and omniselector is anti-in real time
Current location is presented, the intercept net of real time position and the omniselector feedback for the unmanned plane that control system monitor according to early warning system
Real time position makes blocking apparatus appropriate flight attitude adjustment so that intercept net is eventually arrived at unmanned plane；In intercept net
After enwinding unmanned plane, parachute catapult-launching gear starts, and radome fairing is opened, and parachute is ejected, and then entire unmanned plane is blocked
It cuts net to wrap up and slowly land, unmanned plane drops to ground in which can have no damage safety, and entire unmanned plane, which intercepts process, to be terminated.
The utility model has following advantageous effect compared with prior art：
1st, the unmanned plane blocking apparatus of the utility model can either intercept unmanned plane, and can be by the nothing after interception
Man-machine carry out safety landing so as to avoid the damage to unmanned plane, ensures that it can just produce work and use.
2nd, since the unmanned plane after interception steadily lands under the action of parachute, the personnel on ground will not be made
Into injury, so as to ensure that the safety used of the unmanned plane blocking apparatus.
Description of the drawings
Fig. 1 is a kind of stereochemical structure signal of a specific embodiment of unmanned plane blocking apparatus of the utility model
Figure.
Fig. 2 is the fundamental diagram using the unmanned plane intercepting system of the unmanned plane blocking apparatus of the utility model.
Fig. 3 is the structure diagram of rocket launching bullet in Fig. 2.
Fig. 4 is the fundamental diagram of embodiment 2.
Fig. 5 is the fundamental diagram of embodiment 3.
Fig. 6 is the fundamental diagram of embodiment 4.
Specific embodiment
The utility model is described in further detail with reference to embodiment and attached drawing, but the implementation of the utility model
Mode is without being limited thereto.
Embodiment 1
Referring to Fig. 1-Fig. 3, a kind of unmanned plane blocking apparatus of the utility model includes transmitting stent 3, intercept net 4 and more
A rocket launching bullet 5, wherein, the transmitting stent 3 is equipped with the fixed seat 6 identical with 5 quantity of rocket launching bullet, each fixed
A rocket launching bullet 5 is placed on seat 6, the multiple rocket launching bullet 5 is connected to the edge of intercept net 4；The fire
Arrow transmitting bullet 5 includes body, propeller 5-1, the radome fairing 5-2 for being arranged on propeller 5-1 upper ends, is located in radome fairing 5-2
Parachute 5-3, the parachute 5-3 catapult-launching gears being located in radome fairing 5-2 and the omniselector 5- being located on radome fairing 5-2 outer walls
4。
Referring to Fig. 3, the parachute 5-3 catapult-launching gears are located at the lower section of parachute 5-3, including centrally disposed compression
The pulling assembly of spring 5-31 and setting circumferentially, wherein, the lower end of the compressed spring 5-31 is fixed on body, compression
The upper end of spring 5-31 withstands on parachute 5-3 bottoms and in compressive state；The pulling assembly includes electromagnet 5-32 and drawing
One end of ring 5-33, draw ring 5-33 are connect with parachute 5-3, and the ring body of the other end of draw ring 5-33 is sleeved on stretching for electromagnet 5-32
On contracting axis.Under normality, parachute 5-3 is fixed in radome fairing 5-2, elastic force upward compressed spring 5-31 and electromagnet 5-
The effect of the downward pulling force of 32 telescopic shaft and draw ring 5-33 and in force balance state；When parachute 5-3 is needed by bullet
When penetrating, electromagnet 5-32 is powered, and telescopic shaft is made stretching motion and detached with the ring body of draw ring 5-33, the parachute after separation
5-3 is gone out under the action of compressed spring 5-31 elastic force by ejection, is connected between the parachute and body after opening by the 5-34 that restricts
It connects.
Referring to Fig. 3, the radome fairing 5-2 by left and right two and half radome fairing 5-2 be put together, two and half radome fairing 5-2 it
Between be bolted, on radome fairing 5-2 with the corresponding position of bolt be equipped with automatic apparatus to cause bursting.During the motion, when
When radome fairing 5-2 needs are detached with body, bolt disconnection unlocks radome fairing 5-2 by automatic apparatus to cause bursting by igniting automatically,
Two and half radome fairing 5-2 after unlock are moved out and are detached from body automatically, so as to fulfill the separation of radome fairing 5-2.
Referring to Fig. 2, the transmitting stent 3 is equipped with support plate 3-1, passes through company between the fixed seat 6 and support plate 3-1
Extension bar 3-2 connections, the intercept net 4 are supporting on support plate 3-1.By setting the support plate 3-1 that can realize to solid
Reservation 6 is supported and fixed with intercept net 4.
Referring to Fig. 2, universal ball end 3-3 is equipped between the support plate 3-1 and transmitting stent 3, wherein, universal ball end 3-3
In rotor connect with the support plate 3-1.By setting the universal ball end 3-3, fixed seat 6, connecting rod are enabled to
The whole rotation for carrying out any direction of 3-2, intercept net 4 and rocket launching bullet 5, so as to fulfill the adjusting of whole elevation angle posture,
To emit intercept net 4 to specific direction.
Referring to Fig. 2, the connecting rod 3-2 is electric telescopic rod.During work, by the stretching motion for controlling electric telescopic rod
The distance between rocket launching bullet 5 can be adjusted, so that rocket launching bullet 5 can adapt to different size of intercept net 4, it is real
Now various sizes of unmanned plane is intercepted.The electric telescopic rod can have control system 2 to control, so as to according to intercept net
4 size, the length of the adjusting connecting rod 3-2 of adaptability.
Unmanned plane blocking apparatus described in the utility model needs to rely on early warning system 1 at work and control system 2 is common
With the interception task for completing unmanned plane, wherein, the early warning system 1 is made of a small-sized Airborne Early Warning, operation half
Diameter is up to 5 kilometers or so, tranmitting frequency 1200MHZ.It may detect the information such as position and the speed of aircraft.The omniselector 5-
4 be GPS navigation device or Beidou satellite navigation device；The radome fairing 5-2 is made of lightening fire resistant material, in the air landing speed
Spend it is relatively low, can reduce to the greatest extent to ground staff and property threat；The control system 2 is to be positioned over the console on ground, including
Memory for storing data, the controller for operation, the early radar warning for being communicated with early warning system 1 communicate mould
Block, work for the navigation communication module that is communicated with omniselector 5-4 and for remote control propeller 5-1 it is remote
Journey Solid rocket engine module and the control module for electromagnet 5-32, motor 3-6 to be controlled to work, the main body of the control system 2
It can be made of computer, communication module and control module can be implemented according to the prior art.
Referring to Fig. 1-Fig. 3, the operation principle of unmanned plane blocking apparatus of the invention is：
During work, which cooperates with early warning system, control system, common to complete blocking for unmanned plane
The task of cutting, wherein, the early warning system 1 is used for the location information of unmanned plane for detecting and tracking invasion, and information is passed
Give control system 2；The control system 2 is used for the unmanned plane location information sended over according to early warning system 1, and combines and lead
The location information of boat device 5-4 Real-time Feedbacks controls the propeller 5-1 in intercepting system to start and flies to interception target.
Specifically interception process is：After unmanned plane flies into blank pipe no-fly zone, early warning system 1 will detect and track invasion
Unmanned plane location information, and communicate information to control system 2；The control system 2 is sended over according to early warning system 1
Unmanned plane location information, the propeller 5-1 igniting in intercepting system is controlled to start, multiple rocket launching bullets 5 can drive interception
Net 4 goes up to the air, omniselector 5-4 Real-time Feedbacks current location, the real-time position for the unmanned plane that control system 2 is monitored according to early warning system 1
It puts and the real time position of the intercept net 4 of omniselector 5-4 feedbacks, appropriate flight attitude adjustment is made to blocking apparatus so that
Intercept net 4 is eventually arrived at unmanned plane；After intercept net 4 enwinds unmanned plane, parachute 5-3 catapult-launching gears start, radome fairing
5-2 is opened, and parachute 5-3 is ejected, and then entire unmanned plane is intercepted net 4 and wraps up and slowly land, and unmanned plane can have no to damage
Wound safely drops to ground, and entire unmanned plane, which intercepts process, to be terminated.
Embodiment 2
Referring to Fig. 4, the difference lies between the connecting rod 3-2 and transmitting stent 3 with embodiment 1 for the present embodiment
The elevation angle adjusting rod 3-4 for carrying out elevation angle attitude regulation to rocket launching bullet 5 is additionally provided with, elevation angle adjusting rod 3-4 is by electronic
Telescopic rod is formed, wherein, it is rotatablely connected between one end of elevation angle adjusting rod 3-4 and support plate 3-1 or connecting rod 3-2, the other end
It is rotatablely connected between transmitting stent 3.During work, the motor 3-6 in electric telescopic rod drives telescopic rod to make stretching motion, so as to
Support plate 3-1, fixed seat 6, connecting rod 3-2, intercept net 4 and 5 entirety of rocket launching bullet are pulled down or above push away to change
Its whole elevation angle posture；The electric telescopic rod can be controlled by control system 2, nobody is intercepted so as to basis
The orientation of machine and the direction of the launch and posture for automatically regulating intercept net 4, can more accurately and efficiently realize and unmanned plane is blocked
It cuts.
The present embodiment other embodiment other than the above is same as Example 1.
Embodiment 3
Referring to Fig. 5, the difference lies in the rocket launching bullet 5 in the present embodiment is four to the present embodiment with embodiment 2
A, the elevation angle adjusting rod 3-4 is four, is arranged in a one-to-one correspondence between every elevation angle adjusting rod 3-4 and rocket launching bullet 5.Work
It when making, cooperates between four elevation angle adjusting rod 3-4, such as push is moved on an elevation angle adjusting rod 3-4 work, three elevation angle tune
Pole 3-4 makees drop-down movement, and push is moved on two elevation angle adjusting rod 3-4 works for another example, and two elevation angle adjusting rod 3-4 make lower roping
It is dynamic, so as to the adjustment of the elevation angle posture for making any direction whole to rocket launching bullet 5.
The present embodiment other embodiment other than the above is same as Example 2.
Embodiment 4
Referring to Fig. 6, the difference lies in be additionally provided with to drive the present embodiment on the transmitting stent 3 with embodiment 2
Support plate 3-1, connecting rod 3-2, intercept net 4, fixed seat 6 and the whole rotary drive mechanism rotated of rocket launching bullet 5,
The rotary drive mechanism includes the turntable 3-5 being arranged on the transmitting stent 3 and motor 3-6 of driving disc 3-5 rotations,
In, the elevation angle adjusting rod 3-4 is rotatably connected on turntable 3-5.During work, elevation angle adjusting rod 3-4 is driven when turntable 3-5 is rotated
During rotation, since support plate 3-1, connecting rod 3-2, intercept net 4, fixed seat 6 and rocket launching bullet 5 are entirely through universal ball end
3-3 is connect, therefore the entirety can rotate simultaneously with transmitting stent 3, in this way, carrying out the whole posture of multiple rocket launching bullets 5
During adjusting, first pass through rotary drive mechanism and the circle distribution position of multiple rocket launching bullets 5 is adjusted, then recycle one
Whole elevation angle posture is adjusted in root elevation angle adjusting rod 3-4, so as to complete the distribution of 5 any circumference of rocket launching bullet with
And the dual regulation of arbitrary elevation angle posture, therefore regulating effect is good.The motor 3-6 can be controlled by control system 2, so as to
It is enough automatically to adjust posture.
The present embodiment other embodiment other than the above is same as Example 2.
Above-mentioned is the preferable embodiment of the utility model, but the embodiment of the utility model is not by the above
Limitation, other any Spirit Essences without departing from the utility model with made under principle change, modification, replacement, combine, letter
Change, should be equivalent substitute mode, be included within the scope of protection of the utility model.
Claims (9)
1. a kind of unmanned plane blocking apparatus, which is characterized in that including emitting stent, intercept net and multiple rocket launching bullets,
In, the transmitting stent is equipped with the fixed seat identical with rocket launching bullet quantity, and a rocket hair is placed in each fixed seat
Projectile, the multiple rocket launching bullet are connected to the edge of intercept net；The rocket launching bullet includes body, promotes
Device, the radome fairing for being arranged on propeller upper end, the parachute being located in radome fairing, the parachute catapult-launching gear being located in radome fairing
And it is located at the omniselector on rectification cover outer wall.
2. unmanned plane blocking apparatus according to claim 1, which is characterized in that the parachute catapult-launching gear is located at landing
The lower section of umbrella, including the pulling assembly centrally disposed compressed spring and setting circumferentially, wherein, the compressed spring
Lower end is fixed on body, and the upper end of compressed spring withstands on parachute bottom and in compressive state；The pulling assembly includes
Electromagnet and draw ring, one end of draw ring are connect with parachute, and the ring body of the other end of draw ring is sleeved on the telescopic shaft of electromagnet.
3. unmanned plane blocking apparatus according to claim 2, which is characterized in that the radome fairing is by two and half rectifications of left and right
Cover is put together, and is bolted between two and half radome fairings, is equipped with the corresponding position of bolt on radome fairing and draws automatically
Quick-fried device.
4. unmanned plane blocking apparatus according to claim 3, which is characterized in that the transmitting stent is equipped with support plate,
It is connected between the fixed seat and support plate by connecting rod, the intercept net is supporting in support plate.
5. unmanned plane blocking apparatus according to claim 4, which is characterized in that set between the support plate and transmitting stent
There is universal ball end, wherein, the rotor in universal ball end is connect with the support plate.
6. unmanned plane blocking apparatus according to claim 5, which is characterized in that the connecting rod is electric telescopic rod.
7. unmanned plane blocking apparatus according to claim 6, which is characterized in that between the connecting rod and transmitting stent also
Equipped with for snapping into the elevation angle adjusting rod of row elevation angle attitude regulation to rocket launching, the elevation angle adjusting rod is by electric telescopic rod structure
Into, wherein, it is rotatablely connected between one end of elevation angle adjusting rod and support plate or connecting rod, is rotated between the other end and transmitting stent
Connection.
8. unmanned plane blocking apparatus according to claim 7, which is characterized in that the rocket launching bullet is four, described
Elevation angle adjusting rod is four, is arranged in a one-to-one correspondence between every elevation angle adjusting rod and rocket launching bullet.
9. unmanned plane blocking apparatus according to claim 7, which is characterized in that be additionally provided with to drive on the transmitting stent
The rotary drive mechanism that dynamic support plate, connecting rod, intercept net, fixed seat and rocket launching bullet are integrally rotated, the rotation
Driving mechanism includes the turntable being arranged on transmitting stent and the motor of driving disc rotation, wherein, the elevation angle adjusting rod
It is rotatably connected on turntable.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721570195.9U CN207540428U (en) | 2017-11-20 | 2017-11-20 | A kind of unmanned plane blocking apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721570195.9U CN207540428U (en) | 2017-11-20 | 2017-11-20 | A kind of unmanned plane blocking apparatus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207540428U true CN207540428U (en) | 2018-06-26 |
Family
ID=62614436
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721570195.9U Expired - Fee Related CN207540428U (en) | 2017-11-20 | 2017-11-20 | A kind of unmanned plane blocking apparatus |
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| Country | Link |
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| CN (1) | CN207540428U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108981473A (en) * | 2018-07-27 | 2018-12-11 | 广州中国科学院工业技术研究院 | A kind of hold-up interception method of pair of rotor wing unmanned aerial vehicle |
| CN109682257A (en) * | 2018-09-13 | 2019-04-26 | 西安理工大学 | A kind of Cruise Missile Interception device based on netting capture |
| CN110455126A (en) * | 2019-09-04 | 2019-11-15 | 中交遥感天域科技江苏有限公司 | A kind of launching gun barrel and its working method of unmanned plane intercept net bullet |
| CN116212283A (en) * | 2023-03-27 | 2023-06-06 | 北华航天工业学院 | Multi-petal type remote magnetic control fire extinguishing bomb capable of being filled with multiple fire extinguishing agents |
-
2017
- 2017-11-20 CN CN201721570195.9U patent/CN207540428U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108981473A (en) * | 2018-07-27 | 2018-12-11 | 广州中国科学院工业技术研究院 | A kind of hold-up interception method of pair of rotor wing unmanned aerial vehicle |
| CN109682257A (en) * | 2018-09-13 | 2019-04-26 | 西安理工大学 | A kind of Cruise Missile Interception device based on netting capture |
| CN110455126A (en) * | 2019-09-04 | 2019-11-15 | 中交遥感天域科技江苏有限公司 | A kind of launching gun barrel and its working method of unmanned plane intercept net bullet |
| CN116212283A (en) * | 2023-03-27 | 2023-06-06 | 北华航天工业学院 | Multi-petal type remote magnetic control fire extinguishing bomb capable of being filled with multiple fire extinguishing agents |
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| CF01 | Termination of patent right due to non-payment of annual fee |