CN110332855A - A kind of anti-low flyer arrests bullet - Google Patents
A kind of anti-low flyer arrests bullet Download PDFInfo
- Publication number
- CN110332855A CN110332855A CN201910599472.6A CN201910599472A CN110332855A CN 110332855 A CN110332855 A CN 110332855A CN 201910599472 A CN201910599472 A CN 201910599472A CN 110332855 A CN110332855 A CN 110332855A
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- Prior art keywords
- emission part
- bullet
- arrests
- main body
- arrest
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Classifications
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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
- F41H11/02—Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems
- F41H11/04—Aerial barrages
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The invention discloses a kind of anti-low flyers to arrest bullet, including main body, second level body, arrest net, the first emission part, the second emission part and mass block, main cavity is provided in main body, arrest net is arranged in main cavity, the lower section of main body is arranged in second level body, the connecting pin of second level body and main body is provided with mutually matched boss and groove, boss and groove interference fit；The bottom of second level body is provided with the first emission part, the first emission part it is opening down；The side of second level body is provided with the second emission part；Mass block is fixedly connected with the quadrangle of arrest net by traction rope, and mass block is arranged in the second emission part.Anti- low flyer of the invention arrest play structure it is simple, setting rationally, using two-stage separate emit, using mass block tractive force drive arrest net open, to achieve the purpose that arrest unmanned plane, can effectively hit low latitude unmanned plane.
Description
Technical field
The present invention relates to a kind of anti-low flyers to arrest bullet, belongs to air vehicle technique field.
Background technique
Although the development at full speed of the technology of present anti-unmanned plane, current some technologies, which are appointed, so has this
A little problems, such as the method (limited to the unmanned plane effect of individual's establishment) of control is detected, directly (risk is high, for destruction class
Refinement degree, consuming, energy consumption are high), interference obstructs class (effect is limited).With advances in technology, the popularization degree of unmanned plane is increasingly
Height, popular price that several hundred members to thousands of members do not wait also lower and lower using threshold more promote unmanned plane to become people raw
" toy " in work.However people may accidentally bring great while having a taste of high-altitude beautiful scenery to aviation flight
Security risk is especially prohibited in dead zone on airport, if collided during takeoff and landing with unmanned plane, consequence will can't bear to set
Think.Consumer level unmanned plane and technical grade unmanned plane have certain load and cruising ability, if by malicious person in weight
It wants sensitive sites to be used to take on the sly, fear attack, poison, shedding leaflet etc., it will social security and public safety are caused a significant threat.
Unmanned plane detection and counter technology global evolution are unbalance, normal radar detection target be mainly the high-altitudes such as guided missile, aircraft, it is quick,
Big target (referred to as tall and big fast target), unmanned plane in contrast then belong to low latitude, at a slow speed, Small object (referred to as low slow small mesh
Mark), volume is smaller, speed is slower, flying height is lower, and detection difficulty is bigger.The reflection cross section of low slow Small object is very small,
So conventional radar can not be detected effectively, it is easy intrusion no-fly zone and causes major safety risks.
Therefore, propose that a kind of anti-low flyer arrests bullet regarding to the issue above.
Summary of the invention
The object of the invention is that providing a kind of anti-low flyer to solve the above-mentioned problems arrests bullet.
The present invention through the following technical solutions to achieve the above objectives:
A kind of anti-low flyer arrests bullet, including main body, second level body, arrest net, the first emission part, the second transmitting
Portion and mass block；
Main cavity is provided in the main body, the arrest net is arranged in main chamber body,
The second level body is arranged in the lower section of the main body, and the connecting pin of the second level body and the main body is set
It is equipped with mutually matched boss and groove, the boss and groove interference fit；
The bottom of the second level body is provided with the first emission part, first emission part it is opening down；
The side of the second level body is provided with the second emission part；
The mass block is fixedly connected with the quadrangle of the arrest net by traction rope, and mass block setting is described the
In two emission parts.
Further, the opening of second emission part tilts upward.
Further, the quantity of the mass block is four, and four mass blocks pass through traction rope respectively and connect respectively
Connect the quadrangle of the arrest net.
Further, second emission part includes four transmitting tubes, and four mass blocks are separately positioned on four
In the transmitting tube.
Further, the surrounding of the second level body is provided with guide groove.
Further, the quantity of the guide groove is four.
Further, four guide grooves are separately positioned on the surface of four transmitting tubes.
Further, the bottom of the mass block is provided with block.
It further, further include rubber plug, one end of the rubber plug is provided with plug, and the other end and the main body connect
It connects, the opening of second emission part is arranged in the plug.
Inventive principle: anti-low flyer of the invention arrests bullet in use, emitting main body and second level body first,
After main body and the transmitting of second level body, launch mass block when reaching the scheduled time draws exhibition by four mass blocks
Open arrest net, arrest net capture target aircraft.
The utility model has the advantages that anti-low flyer of the invention is arrested, bullet structure is simple, and setting rationally, is separated using two-stage and sent out
It penetrates, drives arrest net to open using the tractive force of mass block, to achieve the purpose that arrest unmanned plane, can effectively hit low latitude
Unmanned plane.
Detailed description of the invention
Fig. 1 is the main view of main body of the invention；
Fig. 2 is the perspective view of second level body of the invention；
Fig. 3 is the cross-sectional view of second level body of the invention；
Fig. 4 is the structural schematic diagram of the first emission part of the invention；
Fig. 5 is the structural schematic diagram that anti-low flyer of the invention arrests bullet；
Fig. 6 is the structural schematic diagram of rubber plug of the invention.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
It please refers to shown in Fig. 1-6, anti-low flyer of the invention arrests bullet, including main body 1, second level body 2, arrests
Net, the first emission part 3, the second emission part 4 and mass block；
Main cavity 11 is provided in main body 1, arrest net 13 is arranged in main cavity 11,
Second level body 2 is arranged in the lower section of main body 1, and the connecting pin of second level body 2 and main body 1 is provided with mutual cooperation
Boss 21 and groove 12, boss 21 and groove 12 are interference fitted；
The bottom of second level body 2 is provided with the first emission part 3, the first emission part 3 it is opening down；
The side of second level body 2 is provided with the second emission part 4；
Mass block is fixedly connected with the quadrangle of arrest net by traction rope, and mass block is arranged in the second emission part 4.
Preferably, the opening of the second emission part 4 tilts upward.When for emitting, made using the reaction force of transmitting tube
The structure of lower two bodies separates, and convenient for the smooth expansion of arrest net, realizes catching function.
Preferably, the quantity of mass block is four, and four mass blocks pass through traction rope is separately connected arrest net four respectively
Angle.
Preferably, the second emission part 4 includes four transmitting tubes, and four mass blocks are separately positioned in four transmitting tubes.Benefit
Separate the structure of upper and lower two bodies with the reaction force of four transmitting tubes, convenient for the smooth expansion of arrest net, realization is arrested
Function.
Preferably, the surrounding of second level body 2 is provided with guide groove 22.
Preferably, the quantity of guide groove 22 is four.
Preferably, four guide grooves 22 are separately positioned on the surface of four transmitting tubes.
Preferably, the bottom of mass block is provided with block.
It preferably, further include rubber plug 5, one end of rubber plug 5 is provided with plug, and the other end is connect with main body 1, plug setting
In the opening of the second emission part 4.Rubber plug can not only block the opening of the second emission part, but also can use it to main bullet
Body and second level body play certain connection function.
Specifically,
One, arrest the main cavity 11 of bullet: main cavity 11 is primarily used to the storage arrest net to be emitted；
Two, it arrests the connecting portion of bullet: after the transmitting of main body 1, completing the separation of main body 1 and second level body 2
Just arrest net can be made smoothly to be unfolded and implement the effect of arresting, in the connecting portion of main body 1 and second level body 2, such as Fig. 1 and figure
Shown in 2: between main body 1 and second level body 2, as long as realizing main 1 He of body using the interference fit of boss 21 and groove 12
Second level body 2 it is circumferentially positioned, make body that circumferential twisting not occur with this.In axially position in order to make body up and down
Two parts can either closely connect and also will be convenient for the later period the second-order separation, we use rubber plug 5, mass block emission port and
Connection is realized between upper body, the quadrangle for drawing arrest net is unfolded, and realizes the function of arresting.
It is as shown in the figure: the upper end of second level body 2 being connect with the lower part of main body 1, is connected by socket mode therebetween
It connects, generated impact force is that two parts body separates up and down when using transmitting.At the same time, the traction of four mass blocks is utilized
Power opens arrest net, to achieve the purpose that arrest unmanned plane.
Three, the transmitting position of bullet: the transmitting problem of body is made to lead first using the principle of two-stage separation transmitting
Body transmitting drives entire body to emit to corresponding height, after the transmission, then the principle of Secondary Emission is used to make second level bullet
Four corresponding mass block transmittings in the transmitting tube of body side surface, are traction with mass block, open arrest net, grab to reach
The effect caught.
It is as shown in Figure 2, Figure 3 and Figure 4: to place corresponding filler, transmitting band in the ammunition filler 31 of the first emission part 3
Move the transmitting of entire body.Gunpowder and emitting substance are placed in the transmitting tube 41 of the second emission part 4, drive four mass blocks
Transmitting, to draw the skyborne opening of arrest net, reaches corresponding catching function with this.
Since mass block is connected with traction rope, in order to guarantee enough impact forces when transmitting, in the bottom of mass block
Corresponding rounded stops are placed, so that possessing the transmitted at high speed that enough thrust guarantees mass block when transmitting.
Inventive principle: anti-low flyer of the invention arrests bullet in use, emitting main body and second level body first,
After main body and the transmitting of second level body, launch mass block when reaching the scheduled time draws exhibition by four mass blocks
Open arrest net, arrest net capture target aircraft.
Anti- low flyer of the invention arrest play structure it is simple, setting rationally, using two-stage separate emit, utilize quality
The tractive force of block drives arrest net to open, to achieve the purpose that arrest unmanned plane, can effectively hit low latitude unmanned plane.
Claims (9)
1. a kind of anti-low flyer arrests bullet, it is characterised in that: including main body (1), second level body (2), arrest net, first
Emission part (3), the second emission part (4) and mass block；
It being provided with main cavity (11) in the main body (1), the arrest net setting is interior in main chamber body (11),
The second level body (2) setting in the lower section of the main body (1), the second level body (2) and the main body (1)
Connecting pin is provided with mutually matched boss (21) and groove (12), the boss (21) and groove (12) interference fit；
The bottom of the second level body (2) is provided with the first emission part (3), first emission part (3) it is opening down；
The side of the second level body (2) is provided with the second emission part (4)；
The mass block is fixedly connected with the quadrangle of the arrest net by traction rope, and the mass block setting is in second hair
It penetrates in portion (4).
2. anti-low flyer according to claim 1 arrests bullet, it is characterised in that: the second emission part (4) are opened
Mouth tilts upward.
3. anti-low flyer according to claim 1 arrests bullet, it is characterised in that: the quantity of the mass block is four
A, four mass blocks pass through the quadrangle that traction rope is separately connected the arrest net respectively.
4. anti-low flyer according to claim 3 arrests bullet, it is characterised in that: second emission part (4) includes
Four transmitting tubes, four mass blocks are separately positioned in four transmitting tubes.
5. anti-low flyer according to claim 4 arrests bullet, it is characterised in that: the surrounding of the second level body (2)
It is provided with guide groove (22).
6. anti-low flyer according to claim 5 arrests bullet, it is characterised in that: the quantity of the guide groove (22) is
Four.
7. anti-low flyer according to claim 6 arrests bullet, it is characterised in that: four guide grooves (22) are respectively
The surface of four transmitting tubes is set.
8. anti-low flyer according to claim 1 arrests bullet, it is characterised in that: the bottom of the mass block is provided with
Block.
9. anti-low flyer according to claim 1 arrests bullet, it is characterised in that: further include rubber plug (5), the rubber plug
(5) one end is provided with plug, and the other end is connect with the main body (1), and the plug is arranged in second emission part (4)
Opening.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910599472.6A CN110332855A (en) | 2019-07-04 | 2019-07-04 | A kind of anti-low flyer arrests bullet |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910599472.6A CN110332855A (en) | 2019-07-04 | 2019-07-04 | A kind of anti-low flyer arrests bullet |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110332855A true CN110332855A (en) | 2019-10-15 |
Family
ID=68144190
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910599472.6A Pending CN110332855A (en) | 2019-07-04 | 2019-07-04 | A kind of anti-low flyer arrests bullet |
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| CN (1) | CN110332855A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114153223A (en) * | 2021-09-22 | 2022-03-08 | 航天科工微电子系统研究院有限公司 | Net type capturing system and method for clustered unmanned aerial vehicle |
| CN114234723A (en) * | 2022-01-12 | 2022-03-25 | 新疆宏开电子系统集成有限公司 | Unmanned aerial vehicle carries on device of physical seizure unmanned aerial vehicle of being exclusively used in |
Citations (3)
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| US20180245888A1 (en) * | 2015-08-27 | 2018-08-30 | Airspace Systems Inc. | Interdiction system and method of operation |
| RU185949U1 (en) * | 2018-10-08 | 2018-12-25 | Федеральное государственное унитарное предприятие "Российский федеральный ядерный центр - Всероссийский научно-исследовательский институт технической физики имени академика Е.И. Забабахина" | DEVICE FOR UNMANNED AERIAL VEHICLES |
| 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 |
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2019
- 2019-07-04 CN CN201910599472.6A patent/CN110332855A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20180245888A1 (en) * | 2015-08-27 | 2018-08-30 | Airspace Systems Inc. | Interdiction system and method of operation |
| 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 |
| RU185949U1 (en) * | 2018-10-08 | 2018-12-25 | Федеральное государственное унитарное предприятие "Российский федеральный ядерный центр - Всероссийский научно-исследовательский институт технической физики имени академика Е.И. Забабахина" | DEVICE FOR UNMANNED AERIAL VEHICLES |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114153223A (en) * | 2021-09-22 | 2022-03-08 | 航天科工微电子系统研究院有限公司 | Net type capturing system and method for clustered unmanned aerial vehicle |
| CN114234723A (en) * | 2022-01-12 | 2022-03-25 | 新疆宏开电子系统集成有限公司 | Unmanned aerial vehicle carries on device of physical seizure unmanned aerial vehicle of being exclusively used in |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20191015 |
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| RJ01 | Rejection of invention patent application after publication |