CN106679507B - One kind is soft to injure ammunition - Google Patents
One kind is soft to injure ammunition Download PDFInfo
- Publication number
- CN106679507B CN106679507B CN201710058059.XA CN201710058059A CN106679507B CN 106679507 B CN106679507 B CN 106679507B CN 201710058059 A CN201710058059 A CN 201710058059A CN 106679507 B CN106679507 B CN 106679507B
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- Prior art keywords
- soft
- bullet
- dictyosome
- unmanned plane
- ammunition
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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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/56—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing discrete solid bodies
- F42B12/58—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles
- F42B12/66—Chain-shot, i.e. the submissiles being interconnected by chains or the like
Abstract
Present invention offer one kind is soft to injure ammunition, and soft bullet of injuring is fixed on dictyosome；Fuse is arranged in dictyosome；Fuse will be used for after detecting UAV targets' distance and velocity information, realize and calculate optimum distance or time by basic point of miss distance, provide activation control information, and activation is soft to injure bullet, while the opening opportunity of umbrella bag is precisely controlled.The present invention solves the propeller type unmanned plane that the net bullet examination hold-up interception method that prior art proposes is only applicable to metal material, not only the unmanned plane target of high-speed maneuver is difficult to precisely catch, and the technical problem of secondary injury is caused to ground staff or other targets.The present invention is highly reliable, because adhesive has very strong sticky and quick coagulability, easy capture target, and can reduce dictyosome area, so as to reduce transmitting difficulty, intelligent detecting and soft seizure can be achieved；And it is safe and reliable during unmanned plane is captured, safe retrieving unmanned plane can be achieved.
Description
Technical field
It is specific that a kind of be used for the anti-nothing of inexpensive Small Civil unmanned plane proposition is provided the present invention relates to anti-unmanned plane field
The soft of man-machine technology injures ammunition.
Background technology
The background of related of the present invention is illustrated below, but these explanations might not form the existing of the present invention
Technology.
In recent years, as unmanned air vehicle technique is constantly ripe, the cost of unmanned plane is more and more lower, more next using the people of unmanned plane
It is more, while bringing efficient operation, convenient life, also bring a series of potential safety hazard.Such as utilize nobody
Machine is taken on the sly national defence important base, scientific research concerning security matters place, no-fly region etc., has what is heard during the news for stealing state secret；Terror point
Son launches dangerous goods using unmanned plane to important base, place or residential block, brings bigger harm.
At present, the domestic anti-unmanned air vehicle technique for inexpensive Small Civil unmanned plane is existing mostly based on seizure
Seizure means are mainly launch network bullet, throw the net and arrest, such as State Intellectual Property Office disclosed applicant on June 29th, 2016
For Shanghai Yi Nai new materials Science and Technology Ltd., Application No. 201610062940.2, a kind of entitled anti-unmanned plane of net bullet formula
The patent of intelligent intercept system, net bullet is projected using fixed launcher or mobile launcher, deploys net when close to unmanned plane
Body, snarl unmanned plane using inertia, the net on netting gear must snarl the propeller of unmanned plane, it is run out of steam, reach seizure nothing
Man-machine effect.But this mode reliability is small, non-directiveness is big, it is difficult to unmanned plane rotating part is snarled, even if holding after snarling
It is easy to fall off, and be only applicable to propeller type unmanned plane, the technical scheme that the document provides is by detection early warning system pair
Early warning is carried out to attack invasion unmanned plane, radar signal is received by ground or aerial control emission system and sends interception instruction, then
Target is arrested by launching intelligent intercept net bullet, intelligent intercept net bullet by discharge transmitting by high-strength high-modulus polyethylene and
The netting gear that intelligent conductive fiber braiding forms, intercepted under the directed traction effect that electromagnetic induction is formed and arrest unmanned plane, and led to
Unmanned plane propeller must be wound by crossing net, it is run out of steam, speed slows down, and is wound and arrests.Adopted although mentioning in the literature
Possess that early warning range is wide, intercept speed is fast, have a wide range of application, hit that accuracy rate is high, intelligent and high-efficiency with above method, can be to opposing
Square unmanned plane carries out effective comprehensive, multi-angle interference, intercepts, arrests, and can be according to unmanned plane in pre-warning signal
Model size, the net bullet of the corresponding netting gear of selection transmitting, so that the advantages of interception result is more preferable.But there is following lack in this mode
Point：
(1) reliability is small, non-directiveness is big, it is difficult to unmanned plane rotating part is snarled, even if easily being come off after snarling.
(2) high is required to pointing accuracy or dictyosome diametric requirements is big.
(3) unmanned plane for being suitable only for propeller type must be wound by netting, and must snarls and capture target using net, it is difficult to
Suitable for harmfulness is big, occasion in critical condition, and secondary injury easily is caused to ground staff or other targets.
(4) it is ground of falling after this method capture target, is more easy to cause secondary injury to ground staff and other targets.
(5) it is unclear that unmanned plane principle is arrested in the directed traction effect interception formed using electromagnetic induction, it is difficult to suitable for non-
The unmanned plane of metal material.
The content of the invention
The net proposed to solve prior art plays the propeller type unmanned plane that hold-up interception method is only applicable to metal material, not only
Easily come off even if being difficult to snarl after unmanned plane snarls, and the technology of secondary injury is easily caused to ground staff or other targets
Problem, the present invention propose that one kind is soft and injure ammunition.
In a preferred embodiment according to the present invention, present invention offer one kind is soft to injure ammunition, wherein soft injure
Ammunition injures bullet, fuse, dictyosome and umbrella bag including soft；Soft bullet of injuring is fixed on dictyosome；Fuse is arranged in dictyosome；
Fuse be used for will detect UAV targets' distance and velocity information after, realize using miss distance as basic point calculate optimum distance or
Time, activation control information is provided, activation is soft to injure bullet, while the opening opportunity of umbrella bag is precisely controlled.
Preferably, above-mentioned soft bullet of injuring is made up of base, spraying device, stay hook, network activation device and calymma；
Its center base is fixedly linked by stay hook and dictyosome；Base is additionally operable to connect calymma, installation spraying device and network activation dress
Put；Fuse is connected by network activation device with the spraying device in each soft destruction bullet；Spraying device uses electric igniter,
Under the control of the active information signal of network activation device, calymma is hit by the energy signal for producing detonation effect
It is broken, erupt adhesive；Calymma is used to store adhesive；Spraying device is controlled by fuse activation control information, through fuse and spray
The adhesive best fit of hair is calculated, and after judging that dictyosome twines and clings unmanned plane, deployment bag is played with the optimum delay time.
Preferably, above-mentioned soft bullet of injuring is multiple；
Preferably, above-mentioned soft bullet of injuring is preferably 24；The corresponding soft network activation device for injuring bullet is 24 tunnels；24
Road network activation device contains 24 spot net active circuits and adaptive delay active circuit；For snarling nobody when dictyosome
During machine so that be wrapped in 24 of diverse location on dictyosome it is soft injure bullet while erupt, wrap up in and twine and cling unmanned plane.
Preferably, above-mentioned fuse is millimeter wave frequency-modulated fuze.
Preferably, sealing container is made by the polythene material of 1-2 millimeters thicks in above-mentioned calymma.
Preferably, above-mentioned adhesive is the instant drying adhesive of 401 or 406 or 502 or 1207 models.
Preferably, above-mentioned diameter 4-10 rice of throwing the net.
Preferably, a diameter of 20-30mm of above-mentioned calymma.
Preferably, above-mentioned preferably 6 meters of diameter of throwing the net.
Specifically advantage is：
1st, it is highly reliable, because adhesive has very strong sticky and quick coagulability, easy capture target, and dictyosome can be reduced
Area, so as to reduce transmitting difficulty, intelligent detecting and soft seizure can be achieved.
2nd, it is safe and reliable during unmanned plane is captured, safety, soft landing recovery unmanned plane can be achieved, for dangerous goods
Secondary injury can be effectively avoided, and is avoided caused by directly crash to ground staff and the secondary injury of other targets.
3rd, the soft ammunition of injuring is applied to capture occasion to polytype unmanned plane such as propeller type, pneumatic type, is applicable
In catching scounting aeroplane, Electronic Warfare UAV, target drone, anti-radiation drone that metal and nonmetallic materials make, attack over the ground
Hit unmanned plane, communication relay unmanned plane, cannon and relatively penetrate unmanned plane, extraordinary unmanned plane, bait unmanned plane, fixed-wing unmanned plane, rotation
The flying objects such as wing unmanned plane, flapping wing unmanned plane, dirigible.
Brief description of the drawings
By that will become more and the specific embodiment part provided, the features and advantages of the present invention referring to the drawings
It is readily appreciated that, in the accompanying drawings：
Fig. 1, which is that the present invention is soft, injures submunition structural representation after dictyosome opening；
Fig. 2 is the soft use state figure for injuring submunition in the present invention.
Fig. 3 is the soft front view for injuring bullet structure schematic diagram in the present invention.
Fig. 4 is the soft left view for injuring bullet structure schematic diagram in the present invention.
Description of reference numerals：1- is soft, and to injure bullet, 2- fuses, 3- dictyosomes, 4- umbrellas bag, 5- bases, 6- spraying devices, 7- solid
Determine hook, 8- network activations device, 9- calymmas.10- searches for head；
11- early warning detection devices；12- launching tubes；13- unmanned plane targets；15- is soft to injure submunition.
Embodiment
The illustrative embodiments of the present invention are described in detail with reference to the accompanying drawings.Illustrative embodiments are retouched
State merely for the sake of demonstration purpose, and be definitely not to the present invention and its application or the limitation of usage.
Shown in Figure 1, soft ammunition 15 of injuring provided by the invention injures bullet 1, fuse 2, dictyosome 3 and umbrella including soft
Bag 4；Soft bullet 1 of injuring is fixed on dictyosome 3；Fuse 2 is arranged in dictyosome 3.The present invention concrete operating principle process referring to
Shown in Fig. 2, search head 10 is loaded on vehicle roof or open-type vehicle carriage, concrete structure be dimensional turntable or universal turning bench or
Spherical electric platform.Dimensional turntable structure, which has, realizes azimuth and angle of pitch function of search；Universal turning bench its table top both can be with
Rotate horizontally, it is also vertically rotating, therefore, can with early warning detection device 11 and launching tube 12 three-dimensional space to target nobody
Machine carries out comprehensive observation；In order to attractive in appearance and hidden, spherical electric platform can be used, when head is in horizontal and vertical two sides
During to any rotating, the movement locus of its early warning detection device 11 and launching tube 12 in front end just forms a sphere, moreover it is possible to carries out
At a high speed, changed speed operation, instant reversal can be steady, noiseless during operation to monitoring unmanned plane fast search and accurate tracking.Three kinds
The search head of structure is realized to nothing by the flexible modulation at azimuth and the angle of pitch to early warning detection device 11 and launching tube 12
The accurate search of man-machine target 13, once unmanned plane target 13 is searched, lockable unmanned plane target 13.Launching tube in the present invention
12 be standard rocket-launching battery, for being calculated according to the given angle of pitch of search head 1, azimuth, and early warning detection device 11
The transmitting of the information such as distance, speed and the angle of the UAV targets gone out is soft to injure submunition 15.Wherein it is soft injure bullet 1 set it is more
Individual, each soft bullet 1 of injuring is made up of base 5, spraying device 6, stay hook 7, network activation device 8, calymma 9, and base 5 passes through
Stay hook 7 is fixedly linked with dictyosome 3, soft bullet 1 of injuring is not come off.Base 5 is additionally operable to connect calymma 9, installation eruption dress
6 and network activation device 8 are put, fuse 2 is connected by network activation device 8 with the spraying device 6 in each soft destruction bullet；Spray
Transmitting apparatus 6 uses electric igniter, under the control of the active information signal of network activation device 8, by producing detonation effect
Energy signal smashes to calymma 9, erupts adhesive；Calymma 9 is used to store adhesive；Spraying device 6 is activated by fuse 2 to be controlled
The control of information processed, calculated through fuse 2 and the adhesive best fit of eruption, after judging that dictyosome 3 twines and clings UAV targets 13,
Deployment bag 4 is beaten with the optimum delay time.The characteristics of wherein electric igniter has wink Fa Dugao, and control accuracy is high, can be by electric control
Signal is changed into the energy signal of detonation.
Referring back to shown in Fig. 1, the fuse 2 in the present invention selects millimeter wave frequency-modulated fuze, is placed in the center of dictyosome 3, is used for
After the distance of UAV targets 13 and velocity information will be detected, realize and calculate optimum distance or time by basic point of miss distance,
Provide activation control information, by the multi-channel network of setting activate device 8 activate respectively it is multiple it is soft injure bullet 1, while to umbrella
The opening opportunity of bag 4 is precisely controlled.Specific implementation is made a reservation for when millimeter wave frequency-modulated fuze detects unmanned plane entrance
During miss distance, the soft bullet 1 of injuring of control erupts adhesive, causes unmanned plane not fly, then opens deployment bag 4, makes what is arrested
Unmanned plane slowly land.In the present embodiment, employ 24 it is soft injure bullet, 24 road networks activation device contains 24 spot nets
Active circuit and adaptive delay active circuit, when dictyosome snarls unmanned plane so that be wrapped in diverse location on dictyosome
24 it is small-bore it is soft injure bullet while erupt, wrap up in and twine and cling unmanned plane.Umbrella bag 4 is specifically controlled by millimeter wave frequency-modulated fuze,
Calculate through fuse and the adhesive best fit of eruption, after judging that dictyosome 3 twines and clings unmanned plane, export optimal to 4 one, umbrella bag
Delay time, after dictyosome, which twines, clings unmanned plane, umbrella bag forms parachute according to the parachute-opening of optimum delay time after umbrella bag parachute-opening,
The unmanned plane for being wrapped up by dictyosome and being clung is dropped into ground slowly, completes soft recovery, safe retrieving process.In this way
It is highly reliable, because adhesive has very strong sticky and quick coagulability, easy capture target, and dictyosome area can be reduced, so as to
Reduce transmitting difficulty.
Shown in Figure 3, base 5 is made up of hard aluminum profile extrusion, plays connection calymma 9, installation spraying device 6 and network and swashs
Removable mounting puts the effect of 8 grades, and can prevent spraying device 6 from producing detonation, erupting backward when smashing calymma 9.Spraying device 6 is used to spray
Adhesive, the electric igniter of standard can be used, under the active information signal control of network activation device 8, produce energy signal.
The energy signal can produce detonation effect, smash calymma 9, erupt adhesive.Each stay hook 7 consolidates each soft destruction bullet 1
It is scheduled on dictyosome 3, millimeter wave frequency-modulated fuze is connected by network activation device 8 with the spraying device 6 in each soft destruction bullet.
The activation control information that millimeter wave frequency-modulated fuze provides, start network activation device 8, make detonation caused by each spraying device 6
Energy smashes calymma 9, adhesive is erupted, so as to activate each soft destruction bullet 1.
Shown in Figure 4, the calymma 9 in the present invention is used to store adhesive, and wherein calymma 9 can be by the poly- of 1-2 millimeters thicks
Vinyl material is made sealing container, and adhesive can use the instant drying adhesive of the models such as 401,406,502 or 1207, in the present embodiment,
It is preferred with 406 instant drying adhesives.When calymma 9 is crashed to pieces, after instant drying adhesive eruption, the 1-2 seconds are curable.Big neglect of the diameter of calymma 9 is opened
Depending on net diameter and launching tube diameter.The present embodiment, so that throw the net 6 meters of diameter, bore is 82mm rocket launchers as an example, calymma diameter
Optional 20-30mm；By it is corrosion resistant, have preferable intensity but be easy to quick-fried broken material and be made, include with very strong viscosity and quick
The adhesive of solidification, it can snarl dictyosome during eruption and cling unmanned plane；Either propeller type unmanned plane, still
Pneumatic type unmanned plane, the adhesive quickly solidified can wrap up and cling whole unmanned plane, it is not flown and reach seizure effect.
Although with reference to illustrative embodiments, invention has been described, but it is to be understood that the present invention does not limit to
The embodiment that Yu Wenzhong is described in detail and shown, in the case of without departing from claims limited range, this
Art personnel can make various improvement or change+type to the illustrative embodiments.
Claims (9)
1. one kind is soft to injure ammunition, it is characterised in that：The soft ammunition of injuring injures bullet, fuse, dictyosome and umbrella including soft
Bag；The soft bullet of injuring is fixed on dictyosome；The fuse is arranged in dictyosome；The fuse be used for will detect target without
After man-machine distance and velocity information, realize and calculate optimum distance or time by basic point of miss distance, provide activation control information,
Activate it is soft injure bullet, while the opening opportunity of umbrella bag is precisely controlled；The soft bullet of injuring is filled by base, eruption
Put, stay hook, network activation device and calymma composition；The base is fixedly linked by stay hook and dictyosome；The base
It is additionally operable to connect calymma, installation spraying device and network activation device；The fuse is killed by network activation device with each soft
The spraying device hindered in bullet is connected；The spraying device uses electric igniter, in the active information signal of network activation device
Control under, calymma is smashed by the energy signal for producing detonation effect, erupt adhesive；The calymma is used to store
Adhesive；The spraying device is controlled by fuse activation control information, is calculated through fuse and the adhesive best fit of eruption,
After judging that dictyosome twines and clings unmanned plane, deployment bag is beaten with the optimum delay time.
2. soft ammunition is injured according to claim 1, it is characterised in that：The soft bullet of injuring is multiple.
3. soft ammunition is injured according to claim 2, it is characterised in that：The soft bullet of injuring is 24；Correspond to soft ruin
The network activation device for hindering bullet is 24 tunnels；24 road networks activation device contains 24 spot net active circuits and adaptive and prolonged
When active circuit；For when dictyosome snarls unmanned plane so that being wrapped in 24 of diverse location on dictyosome, soft to injure bullet same
When erupt, wrap up in and twine and cling unmanned plane.
4. soft ammunition is injured according to claim 3, it is characterised in that：The fuse is millimeter wave frequency-modulated fuze.
5. soft ammunition is injured according to claim 4, it is characterised in that：The calymma by 1-2 millimeters thicks polyethylene material
Sealing container is made in material.
6. soft ammunition is injured according to claim 5, it is characterised in that：Adhesive is 401 or 406 or 502 or 1207 types
Number instant drying adhesive.
7. soft ammunition is injured according to claim 6, it is characterised in that：The diameter 4-10 rice of throwing the net of the dictyosome.
8. soft ammunition is injured according to claim 7, it is characterised in that：The a diameter of 20-30mm of calymma.
9. soft ammunition is injured according to claim 8, it is characterised in that：6 meters of the diameter of throwing the net of the dictyosome.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201710058059.XA CN106679507B (en) | 2017-01-23 | 2017-01-23 | One kind is soft to injure ammunition |
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| CN201710058059.XA CN106679507B (en) | 2017-01-23 | 2017-01-23 | One kind is soft to injure ammunition |
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| CN106679507A CN106679507A (en) | 2017-05-17 |
| CN106679507B true CN106679507B (en) | 2018-04-03 |
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Families Citing this family (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018129612A1 (en) * | 2017-01-10 | 2018-07-19 | AIRSHARE, Inc. | System and method for communicating with a uav |
| CN107014255B (en) * | 2017-05-24 | 2018-09-28 | 大鹏高科（武汉）智能装备有限公司 | A kind of method and apparatus of auxiliary unmanned boat capture unmanned plane |
| CN108088313A (en) * | 2017-11-20 | 2018-05-29 | 华南农业大学 | A kind of unmanned plane intercepting system |
| IL258077B (en) | 2018-03-13 | 2021-02-28 | Elta Systems Ltd | Drone interceptor system, and methods and computer program products useful in conjunction therewith |
| 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 |
| CN110553548A (en) * | 2019-08-30 | 2019-12-10 | 江西洪都航空工业集团有限责任公司 | anti-unmanned aerial vehicle system based on fixed wing platform |
| RU2744227C1 (en) * | 2020-03-23 | 2021-03-03 | ФЕДЕРАЛЬНОЕ ГОСУДАРСТВЕННОЕ КАЗЕННОЕ ВОЕННОЕ ОБРАЗОВАТЕЛЬНОЕ УЧРЕЖДЕНИЕ ВЫСШЕГО ОБРАЗОВАНИЯ "Военная академия Ракетных войск стратегического назначения имени Петра Великого" МИНИСТЕРСТВА ОБОРОНЫ РОССИЙСКОЙ ФЕДЕРАЦИИ | Grenade launcher ammunition against unmanned aerial vehicles |
| CN116379841A (en) * | 2023-03-20 | 2023-07-04 | 中国人民武装警察部队指挥学院 | Capturing type anti-unmanned aerial vehicle interception system and application method thereof |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101982720B (en) * | 2010-09-29 | 2012-11-14 | 北京机械设备研究所 | Interception method of low-altitude low-velocity small targets |
| CN102338596A (en) * | 2011-10-24 | 2012-02-01 | 王海鹏 | Defense weapon for aerospace vehicle |
| DE102015003324A1 (en) * | 2015-03-17 | 2016-09-22 | Diehl Bgt Defence Gmbh & Co. Kg | Projectile for catching a small drone |
| CN105651120A (en) * | 2016-01-30 | 2016-06-08 | 上海仪耐新材料科技有限公司 | Fixed type unmanned aerial vehicle resisting intercept net system |
| CN205602150U (en) * | 2016-01-30 | 2016-09-28 | 上海仪耐新材料科技有限公司 | Anti - unmanned aerial vehicle of net bullet formula intelligence interception system |
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Effective date of registration: 20211220 Address after: 241002 room 1502, 15 / F, building 3, information industry park, high tech Zone, Yijiang District, Wuhu City, Anhui Province Patentee after: Wuhu Tianbo Photoelectric Technology Research Institute Co.,Ltd. Address before: 241000 Wuhu City, Anhui Province 15 / F, building 3, phase II, Service Outsourcing Industrial Park, high tech Industrial Development Zone, Yijiang District, Wuhu City, Anhui Province Patentee before: WUHU BOGAO PHOTOELECTRIC TECHNOLOGY CO.,LTD. |