CN111380407A - Low-slow small target safety interception device - Google Patents
Low-slow small target safety interception device Download PDFInfo
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- CN111380407A CN111380407A CN202010134784.2A CN202010134784A CN111380407A CN 111380407 A CN111380407 A CN 111380407A CN 202010134784 A CN202010134784 A CN 202010134784A CN 111380407 A CN111380407 A CN 111380407A
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- low
- air bag
- interception
- intercepting
- slow small
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- 230000005284 excitation Effects 0.000 claims abstract description 23
- 239000007789 gas Substances 0.000 claims description 25
- 238000012544 monitoring process Methods 0.000 claims description 22
- 238000010304 firing Methods 0.000 claims description 11
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 6
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 claims description 6
- 230000001133 acceleration Effects 0.000 claims description 6
- 229910052734 helium Inorganic materials 0.000 claims description 4
- 239000001307 helium Substances 0.000 claims description 4
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 claims description 4
- 229910002092 carbon dioxide Inorganic materials 0.000 claims description 3
- 239000001569 carbon dioxide Substances 0.000 claims description 3
- 229910052757 nitrogen Inorganic materials 0.000 claims description 3
- 230000001788 irregular Effects 0.000 claims description 2
- 238000000034 method Methods 0.000 abstract description 17
- WABPQHHGFIMREM-UHFFFAOYSA-N lead(0) Chemical compound [Pb] WABPQHHGFIMREM-UHFFFAOYSA-N 0.000 abstract description 7
- 238000004880 explosion Methods 0.000 abstract description 3
- 238000009434 installation Methods 0.000 description 4
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical group C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 1
- 239000002657 fibrous material Substances 0.000 description 1
- 239000012634 fragment Substances 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 230000002452 interceptive effect Effects 0.000 description 1
- 229920001778 nylon Polymers 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 230000035945 sensitivity Effects 0.000 description 1
Images
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
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- General Engineering & Computer Science (AREA)
- Air Bags (AREA)
Abstract
The invention provides a low-slow small target security interception device. The device comprises an intercepting net, an excitation device and at least one automatic air bag; automatic gasbag is aerifyd by lead wire tractive control, automatic gasbag and excitation device are fixed on the interception net, work as when low-altitude aircraft ware intercepting device intercepts the aircraft, aerify through excitation device and lead wire control automatic gasbag, utilize the aerated gasbag bag can effectively reduce the impact force when the interception net falls to the ground, also can slow down the falling speed of aircraft interception net, can effectively prevent secondary disasters such as aircraft explosion, protect ground personnel and facility safety, solved the safety problem that current interception method can't solve. The method is easy to implement, high in reliability and wide in application prospect.
Description
Technical Field
The invention relates to a low-speed small target safety interception device, which mainly relates to the technologies of automatic control, machinery and the like.
Background
The low-slow small target refers to a low-altitude, slow and small aircraft, including rotor unmanned aerial vehicles, fixed-wing unmanned aerial vehicles, balloons and other aircrafts, which have low flying altitude, small volume and low cost and are widely popularized and used in the world, but the aircrafts also pose great threats to the safety management of the airspace. At present, the common intercepting methods for low-speed small targets include firepower interception, laser attack, radio interception, radio interference, unmanned aerial vehicle countermeasure, an intercepting network and the like. Firepower interception is to use weapons such as rocket projectiles and light guided missiles to strike small low-speed targets, but weapon ammunitions have great destructiveness, and ammunition and aircraft fragments are easy to damage ground personnel and facilities, so that the firepower interception can be used only in open and unmanned areas; the laser striking is to burn the parts of the unmanned aerial vehicle by adopting a laser weapon so as to lead the unmanned aerial vehicle to fall; the radio interception is to control the unmanned aerial vehicle to land by adopting the same flight control signal as the unmanned aerial vehicle on the basis of radio interference, and the method is only suitable for part of specific unmanned aerial vehicles with known models; the radio interference is to make the unmanned aerial vehicle lose control of falling by interfering and suppressing radio flight control signals of the aircraft, and the method is only suitable for the aircraft using radio flight control and cannot intercept the aircraft with autonomous navigation function; the unmanned aerial vehicle countermeasure is that the unmanned aerial vehicle with larger volume directly intercepts or impacts the target aircraft in a self-injurious way, and the unmanned aerial vehicle for countermeasure and the target aircraft are crashed on the ground after interception; the interception net can make the aircraft lose the flight ability by throwing the interception net. Except that the radio interception can control the soft landing of the unmanned aerial vehicle, the existing other interception methods can not control the falling process and the falling place of the intercepted aircraft, and the aircraft is easy to cause the explosion of a power system and secondary disasters due to the strong collision with the ground when crashed, thereby causing serious threats to the safety of ground personnel and facilities. In order to solve the problem, part of the intercepting nets are additionally provided with parachutes, but the parachute opening speed is low, the parachute is not opened yet and the aircraft falls down to the ground, and the reliability is poor. Therefore, a new intercepting method and device capable of effectively preventing low-speed small targets from intercepting secondary disasters are needed.
Disclosure of Invention
The invention provides a low-slow small target intercepting device, which comprises an intercepting net, an excitation device and at least one automatic air bag, wherein the intercepting net is arranged on the intercepting net; the automatic air bag and the excitation device are fixed on the intercepting net and are connected through a lead; the automatic air bag comprises an inflating device and an air bag; the excitation device is used for monitoring the state of the intercepting net capturing the low and slow small targets, when the low and slow small targets are monitored to be captured, the lead is automatically pulled, and the inflation device is controlled to inflate the air bag with gas, so that the air bag is expanded.
1. The low-slow small target security interception device further comprises: the inflation device comprises a shell, a gas cylinder plug, a firing pin, a return spring and a rotating wheel; the shell is provided with an inflation inlet which is connected with the air bag; the gas bottle is arranged in the shell, compressed gas is stored in the gas bottle, and the gas bottle is sealed by a gas bottle plug; the firing pin is used for puncturing the air bottle plug and resets under the action of the reset spring after puncturing the air bottle plug; the rotating wheel is in an irregular shape with bulges and is connected with the lead, and when the lead is pulled, the bulge part of the rotating wheel pushes the firing pin to pierce the plug of the air bottle so as to release compressed air in the air bottle and fill the air bag from the inflating port.
2. The low-slow small target security interception device further comprises: the excitation device comprises a switch, an interception net monitoring sensor, a power supply, a relay and a traction motor; the intercepting net monitoring sensor is used for monitoring the state of the intercepting net capturing low and slow small targets, and monitoring signals comprise one or more signals of vibration, deformation, light and acceleration; the sensor comprises an electronic sensor or a mechanical sensor; the lead is wound on the rotating shaft of the traction motor, and when the rotating shaft rotates, the lead is pulled, so that the inflation device is controlled to inflate the air bag, and the air bag is expanded.
3. The low-slow small target security interception device further comprises: the intercepting net monitoring sensor of the excitation device comprises a timing trigger element for recording the throwing time of the intercepting net, and when the timing time reaches the set time, the automatic control inflation device inflates air into the air bag.
4. The low-slow small target security interception device further comprises: the compressed gas comprises carbon dioxide, nitrogen or helium.
The low-slow small-target safety intercepting device effectively reduces impact force when the intercepting net falls to the ground by utilizing the inflatable airbag, and as the airbag increases the section area of the intercepting net, the falling speed of the aircraft intercepting net can also be reduced, secondary disasters such as aircraft explosion can be effectively prevented, ground personnel and facility safety are protected, and the safety problem which cannot be solved by the existing intercepting method is solved. The method is easy to implement, high in reliability and wide in application prospect. In the intercepting process, the intercepted target is easy to pull the lead wire, so that the automatic air bag is directly excited to rapidly expand the air bag, the expanded air bag can further change vibration signals, deformation signals, optical signals or acceleration signals, the intercepting net monitoring sensor is ensured to capture signal changes, and the rest automatic air bags are excited, so that the low-speed small target safety intercepting device has higher sensitivity, accuracy and reliability.
Drawings
Fig. 1 is a schematic view of a low-speed small object intercepting device installation.
Fig. 2 is a schematic diagram of the operation of the low-slow small target intercepting device.
Fig. 3 is a schematic diagram of the working structure of the low-slow small target intercepting device.
FIG. 4 is a schematic view of the inflator.
Fig. 5 is a schematic flow chart of the low-slow small target intercepting device.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying 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 application.
The installation method of the low-slow small target intercepting device is shown in fig. 1, and in this example, the device comprises 4 automatic air bags installed at the edge of the intercepting net and an excitation device installed in the middle of the intercepting net, and the specific steps are as follows:
1. the interception net (101) adopts high-strength nylon fiber materials as net ropes.
2. The automatic air bag (102) is fixedly arranged on the intercepting net, the installation number of the automatic air bag is determined according to the size of the intercepting net, the automatic air bag comprises an inflating device and an air bag, before the intercepting device is used, gas in the air bag is discharged, the automatic air bag is fixed after being folded, and the used device for fixing the air bag does not influence the expansion of the air bag. The working principle of the automatic airbag is explained in detail in the description of fig. 3 and 4.
3. And the excitation devices (103) are fixedly arranged on the intercepting net, and the installation number of the automatic air bags is determined according to the size of the intercepting net. The working principle of the excitation device is explained in detail in the description of fig. 3.
4. And the lead (104) is mainly used for connecting the excitation device and the automatic air bag, and the excitation device is used for dragging the automatic air bag to inflate.
The working schematic of the low-slow small target intercepting device for intercepting the aircraft is shown in fig. 2, when the device intercepts and winds the low-slow small target (202), the exciting device (103) controls the inflating device to inflate the airbag, and the airbag (201) is shown as the effect of the inflated airbag.
The working structure of the low-slow small object intercepting device is shown in fig. 3, and in order to illustrate the connection relationship between the excitation device (103) and the plurality of automatic air bags, the example is illustrated by 2 automatic air bags. All the electric elements of the low-slow small object intercepting device are connected with the power supply in common, and detailed description is omitted in the illustration.
1. The switch (301) is in charge of switching control over the power supply (304), the switch is a normally closed contact switch, when the interception net is not opened, a contact end of the switch is closed, and the power supply is closed and does not supply power; when the interception net is opened, the switch contact end is opened, and the power supply supplies power. When multiple excitation devices (103) are employed, each excitation device shares a switch to reduce device mass.
2. The sensor (302) is the intercepting net monitoring sensor and is used for monitoring the state of the intercepting net captured low-altitude aircraft and controlling the relay to work according to the monitoring result, the monitoring signal comprises one or more signals of vibration, deformation, light and acceleration, and a vibration sensor, a film pressure sensor, a light induction sensor or an acceleration sensor can be adopted; the sensor may be an electronic or mechanical sensor. When the used interception net monitoring sensor is a sensor module for outputting switching value, the interception net monitoring sensor can be directly connected with a relay; when a sensor for outputting digital or analog signals is adopted, a processor is needed to process the signals, and when the monitored signal change meets the set condition, the processor outputs a switch signal to control the relay to work; when various sensors are used, the processor comprehensively processes various signals, and when the monitored signal change meets the set condition, the processor outputs a switch signal to control the relay to work. The interception net monitoring sensor can also adopt timing triggering, and when the timing time reaches the set time, the relay is controlled to work.
3. The relay (303) is used for controlling the traction motor (304), the control end of the relay is connected with the sensor (302), the normally open end of the controlled end of the relay is connected with the positive pole of a power supply, and the common end of the relay is connected with the positive pole of a control line of the traction motor.
4. And the lead is wound on the rotating shaft of the traction motor (304), the rotating shaft rotates when the relay controls the electrification, and the rotating shaft pulls the lead.
5. A power supply (305) comprising a battery and a DC/DC transformer which converts the battery voltage to the voltage required for operation of the sensor (302) power supply and relay (303) control terminals and the traction motor (304).
6. And the inflating device (306) is connected with the excitation device through a lead wire, and the specific structure is specifically illustrated in the description of FIG. 4.
7. The air inlet of the air bag (201) is connected with the inflation inlet of the inflation device (306).
The structure of the inflator is shown in fig. 4, and the specific structure comprises: the gas cylinder comprises a shell (401), a gas cylinder (402), a gas cylinder plug (403), an inflation inlet (404), a firing pin (405), a sealing ring (406), a return spring (407), a rotating wheel (408) and a rotating shaft (409). Compressed gas of carbon dioxide, nitrogen or helium is filled in the gas cylinder; the reel connects lead wire (104) in the figure, when the lead wire was pull, the runner revolved 90 degrees clockwise around the axis of rotation, and the runner bulge can oppress the firing pin rebound at this in-process to puncture the air bottle plug, when the runner rotated 90 degrees, the firing pin was no longer oppressed to the runner, and the firing pin gets back to the normal position under reset spring effect, and the sealed circle also gets back to the airtight firing pin hole of normal position, and the air cylinder mouth has been opened this moment, and the gas in the air cylinder can only be discharged through the inflation inlet, thereby fills into the gasbag.
The work flow of the low-slow small target intercepting device is shown in fig. 5, and specifically includes:
(501), the low-slow small target intercepting device is squeezed in a shrinking mode in a limited space, due to squeezing, a switch contact end of the excitation device is in a closed state, and a power supply is in a power-off and non-power-supply state. When the low-slow small target is found, the low-slow small target intercepting device is ejected or thrown out of the limited space by specific equipment or people.
(502), the intercepting net of the low-slow small target intercepting device is opened in the flying process, the switch contact end of the exciting device is opened, and the power supply starts to supply power to the sensor and the relay.
(503), when the low-slow small target intercepting device meets a flying target, a propeller or other parts of the aircraft can be wound, so that the aircraft loses flying power, and interception is realized.
(504), the motion state of the low-slow small target intercepting device changes when the low-slow small target is intercepted, and the vibration signal, the deformation signal, the light signal or the acceleration signal is obviously changed. The interception net monitoring sensor senses the signal change and sends a control signal to the relay.
And 5, (505) the relay supplies power to the traction motor through the control line under the control of the interception net monitoring sensor, so that the traction motor rotates, and the rotating shaft of the traction motor pulls the lead.
And (506) exciting the inflating device to rapidly inflate gas into the airbag by the pulled lead wire so as to expand the airbag.
(507) the low slow small target intercepting device carries the intercepted low slow small target to land on the ground under the action of gravity. In the descending process, because the expanded air bag effectively increases the section area of the device, the descending speed can be reduced, and if the air bag is filled with light gas such as helium, the descending speed can be further reduced.
Claims (4)
1. Low little target safety interception device slowly, its characterized in that: the device comprises an intercepting net, an excitation device and at least one automatic air bag; the automatic air bag and the excitation device are fixed on the intercepting net and are connected through a lead; the automatic air bag comprises an inflating device and an air bag; the excitation device is used for monitoring the state of the intercepting net capturing the low and slow small targets, when the low and slow small targets are monitored to be captured, the lead is automatically pulled, and the inflation device is controlled to inflate the air bag with gas, so that the air bag is expanded.
The inflation device comprises a shell, a gas cylinder plug, a firing pin, a return spring and a rotating wheel; the shell is provided with an inflation inlet which is connected with the air bag; the gas bottle is arranged in the shell, compressed gas is stored in the gas bottle, and the gas bottle is sealed by a gas bottle plug; the firing pin is used for puncturing the air bottle plug and resets under the action of the reset spring after puncturing the air bottle plug; the rotating wheel is in an irregular shape with bulges and is connected with the lead, and when the lead is pulled, the bulge part of the rotating wheel pushes the firing pin to pierce the plug of the air bottle so as to release compressed air in the air bottle and fill the air bag from the inflating port.
2. The low-slow small-target security interception device according to claim 1, wherein: the excitation device comprises a switch, an interception net monitoring sensor, a power supply, a relay and a traction motor; the intercepting net monitoring sensor is used for monitoring the state of the intercepting net capturing low and slow small targets, and monitoring signals comprise one or more signals of vibration, deformation, light and acceleration; the sensor comprises an electronic sensor or a mechanical sensor; the lead is wound on the rotating shaft of the traction motor, and when the rotating shaft rotates, the lead is pulled, so that the inflation device is controlled to inflate the air bag, and the air bag is expanded.
3. The low-slow small-target security interception device according to claim 2, wherein: the intercepting net monitoring sensor of the excitation device comprises a timing trigger element for recording the throwing time of the intercepting net, and when the timing time reaches the set time, the automatic control inflation device inflates air into the air bag.
4. The low-slow small-target security interception device according to claim 1, wherein: the compressed gas comprises carbon dioxide, nitrogen or helium.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010134784.2A CN111380407A (en) | 2020-03-02 | 2020-03-02 | Low-slow small target safety interception device |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010134784.2A CN111380407A (en) | 2020-03-02 | 2020-03-02 | Low-slow small target safety interception device |
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| CN111380407A true CN111380407A (en) | 2020-07-07 |
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| CN202010134784.2A Pending CN111380407A (en) | 2020-03-02 | 2020-03-02 | Low-slow small target safety interception device |
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Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5583311A (en) * | 1994-03-18 | 1996-12-10 | Daimler-Benz Aerospace Ag | Intercept device for flying objects |
| CN101392999A (en) * | 2007-09-18 | 2009-03-25 | 中国科学院力学研究所 | Aeromodelling interception method and device |
| CN106767172A (en) * | 2017-01-23 | 2017-05-31 | 芜湖博高光电科技股份有限公司 | A kind of pickaback portable anti-unmanned aerial vehicle ejecting is soft to injure retracting device |
| CN206691345U (en) * | 2017-04-28 | 2017-12-01 | 夏慧忠 | The safe school bag of inflatable lifesaving |
| CN212300110U (en) * | 2020-03-02 | 2021-01-05 | 中国矿业大学(北京) | Low-slow small target safety interception device |
-
2020
- 2020-03-02 CN CN202010134784.2A patent/CN111380407A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5583311A (en) * | 1994-03-18 | 1996-12-10 | Daimler-Benz Aerospace Ag | Intercept device for flying objects |
| CN101392999A (en) * | 2007-09-18 | 2009-03-25 | 中国科学院力学研究所 | Aeromodelling interception method and device |
| CN106767172A (en) * | 2017-01-23 | 2017-05-31 | 芜湖博高光电科技股份有限公司 | A kind of pickaback portable anti-unmanned aerial vehicle ejecting is soft to injure retracting device |
| CN206691345U (en) * | 2017-04-28 | 2017-12-01 | 夏慧忠 | The safe school bag of inflatable lifesaving |
| CN212300110U (en) * | 2020-03-02 | 2021-01-05 | 中国矿业大学(北京) | Low-slow small target safety interception device |
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