CN106839898B - Rocket assist formula intelligence suspension bullet system - Google Patents
Rocket assist formula intelligence suspension bullet system Download PDFInfo
- Publication number
- CN106839898B CN106839898B CN201710170472.5A CN201710170472A CN106839898B CN 106839898 B CN106839898 B CN 106839898B CN 201710170472 A CN201710170472 A CN 201710170472A CN 106839898 B CN106839898 B CN 106839898B
- Authority
- CN
- China
- Prior art keywords
- rotor
- accommodating cavity
- suspension bullet
- module
- intelligent
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- 239000000725 suspension Substances 0.000 title claims abstract description 64
- 238000011835 investigation Methods 0.000 claims abstract description 20
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 12
- 238000000926 separation method Methods 0.000 claims description 10
- 238000004891 communication Methods 0.000 claims description 7
- 230000005611 electricity Effects 0.000 claims description 5
- 230000006978 adaptation Effects 0.000 claims description 4
- 238000007667 floating Methods 0.000 abstract description 8
- 230000009286 beneficial effect Effects 0.000 abstract description 4
- 239000003721 gunpowder Substances 0.000 description 3
- 239000003380 propellant Substances 0.000 description 3
- 230000001934 delay Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000004888 barrier function Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000000151 deposition Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/02—Stabilising arrangements
- F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
-
- 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
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
Abstract
The invention provides a kind of rocket assist formula intelligence suspension bullet system, including boost motor and intelligent suspension bullet, the boost motor to include assist device；The intelligent suspension bullet includes power plant module, electrical module, operation module, and the power plant module includes the first rotor and the second rotor reversely rotated each other, and the 3rd rotor of responsible offset distance；The electrical module includes the control circuit of intelligent suspension bullet；The operation module includes injuring load and is responsible for the camera of investigation.The beneficial effects of the present invention are：A kind of intelligent floating type ammunition that can be launched with launching tube is provided, intelligent floating type ammunition is sent to battlefield overhead using boost motor, carry out overlooking investigation using the investigation equipment of its carrying or perform military mission using the ammunition of its carrying, the difficulty that soldier assaults fortified position is substantially reduced, reduces casualty rate.
Description
Technical field
The present invention relates to unmanned plane field, refers in particular to a kind of rocket assist formula intelligence suspension bullet system.
Background technology
In modern war, infantry's street fighting used when fighting it is straight take aim at ammunition, have that the hang time is short, Map and image database is difficult
Shortcoming, and easily stick one's chin out, thus according to needs, there is unmanned plane accessory system, but existing individual soldier patrols winged weapon
Substantially Fixed Wing AirVehicle can not hover on one point, it is necessary to there is certain speed just to stay in the air, during to target observations only
Energy circuit, is extremely limited for the investigation ability in narrow and small street lane.And when striking target, unmanned plane also needs to make larger
Maneuver, easily cause enemy to pay attention to, take workaround in time, it is invalid to cause to attack.
Therefore, it is necessary to which designing a kind of can provide target capability after scouting building or barrier for infantry and possess vertically
The floating type ammunition of striking capabilities.
The content of the invention
The technical problems to be solved by the invention are：A kind of infantry is provided to realize investigation in short-distance and medium-distance street fighting and possess
The ammunition outfit of vertical striking capabilities.
In order to solve the above-mentioned technical problem, the technical solution adopted by the present invention is：A kind of rocket assist formula intelligence suspension bullet
System, including boost motor and intelligent suspension bullet, the boost motor include assist device and boost motor shell, and the assist device is set
One end of the boost motor shell is placed in, the both ends of the boost motor shell are provided with opening, middle to play accommodating cavity formed with suspending,
The intelligent suspension bullet is separably arranged in the suspension bullet accommodating cavity of the boost motor shell；
The intelligent suspension bullet includes power plant module, electrical module, operation module,
The power plant module includes pedestal, the first rotor, the second rotor and the 3rd rotor, first rotor and the second rotation
The wing is arranged on the pedestal, and the 3rd rotor is arranged at one end of the pedestal, first rotor and the second rotor
Rotating shaft is perpendicular to horizontal plane, and the shaft parallel of the 3rd rotor is in horizontal plane；
The electrical module includes electrical enclosure, battery and control circuit, and the both ends of the electrical part shell are provided with opening,
It is middle to be arranged at formed with electric accommodating cavity, the battery and control circuit in the electric accommodating cavity；
The operation module includes operation cabin and investigation cabin, ammunition accommodating cavity, the investigation cabin being provided with the operation cabin
It is interior to be provided with camera；
The other end of one end of the electrical enclosure of the electrical module and the pedestal of power plant module connects, the electrical enclosure
The other end be connected with the other end in the operation cabin of the operation module.
Further, the first rotor of the power plant module of the intelligent suspension bullet includes the first propeller hub and be oppositely arranged two
Piece forward direction blade；
Second rotor includes the second propeller hub and the reverse blade of two panels being oppositely arranged；
3rd rotor includes the 3rd propeller hub and the blade of two panels the 3rd being oppositely arranged.
Further, the positive blade is articulated with the first propeller hub, and the positive blade can be to the electricity of the electrical module
Gas shell direction rotates；The reversely blade is articulated with the second propeller hub, and described reversely blade can be to the electric of the electrical module
Shell direction rotates；3rd blade is articulated with the 3rd propeller hub.
Further, the first rotor of the power plant module of the intelligent suspension bullet and the second rotor wing rotation are in opposite direction.
Further, the outside of the electrical enclosure of the electrical module of the intelligent suspension bullet is convex provided with four along its length
Bar, the raised line are provided with communication antenna.
Further, the other end of the electrical enclosure of the electrical module of the intelligent suspension bullet is provided with internal thread, the work
The one end in the operation cabin for module of fighting is provided with the external screw thread of adaptation.
Further, the both ends of the assist device of the boost motor are provided with opening, and the opening of assist device one end is connected with
First accommodating cavity, the opening of the other end are connected with the second accommodating cavity, wherein, the first accommodating cavity is provided with ejection section, the second accommodating cavity
Provided with separation unit, the separation unit includes mobilizable top and moves back piston, and one end that piston is moved back on the top is provided with groove, and the other end is set
There is opening, the piston accommodating cavity of internal piston moves back on top in the opening UNICOM.
Further, the 3rd accommodating cavity is provided between two accommodating cavities of the assist device, the 3rd accommodating cavity connects
Logical first accommodating cavity and the second accommodating cavity.
Further, the outside of the assist device is provided with some wing plates along its length.
The beneficial effects of the present invention are：A kind of intelligent floating type ammunition that launching tube can be used to launch is provided, using helping
Intelligent floating type ammunition is sent to battlefield overhead by thruster, is carried out overlooking investigation using the investigation equipment of its carrying or is taken using it
The ammunition of band performs military mission, substantially reduces the difficulty that soldier assaults fortified position, reduces casualty rate.
Brief description of the drawings
The concrete structure of the present invention is described in detail below in conjunction with the accompanying drawings：
Fig. 1 is the structural representation of the rocket assist formula intelligence suspension bullet system of the present invention；
Fig. 2 is the structural representation of the assist device of the rocket assist formula intelligence suspension bullet system of the present invention；
Fig. 3 is the structural representation of the power plant module of the rocket assist formula intelligence suspension bullet system of the present invention；
Fig. 4 is the structural representation of the electrical module of the rocket assist formula intelligence suspension bullet system of the present invention；
Fig. 5 is the structural representation of the operation module of the rocket assist formula intelligence suspension bullet system of the present invention；
1- assist devices；The accommodating cavities of 101- first；The accommodating cavities of 102- second；The accommodating cavities of 103- the 3rd；104- moves back piston in top；
105- piston accommodating cavities；
2- boost motor shells；
3- power plant modules；301- pedestals；The rotors of 302- first；The rotors of 303- second；The rotors of 304- the 3rd；305- forward oars
Piece；The reverse blades of 306-；
4- electrical modules；401- raised lines；The electric accommodating cavities of 402-；403- control circuits；
5- operation modules；501- investigates equipment；502- cameras；503- ammunition load.
Embodiment
To describe the technology contents of the present invention, construction feature, the objects and the effects in detail, below in conjunction with embodiment
And accompanying drawing is coordinated to be explained in detail.
Refer to Fig. 1 to Fig. 5, a kind of rocket assist formula intelligence suspension bullet system, including boost motor and intelligent suspension bullet, institute
Stating boost motor includes assist device 1 and boost motor shell 2, and the assist device 1 is arranged at one end of the boost motor shell 2,
The both ends of the boost motor shell 2 are provided with opening, and middle to play accommodating cavity formed with suspending, the intelligent suspension bullet is separably set
It is placed in the suspension bullet accommodating cavity of the boost motor shell 2；
The intelligent suspension bullet includes power plant module 3, electrical module 4, operation module 5,
The power plant module 3 includes pedestal 301, the first rotor 302, the second rotor 303 and the 3rd rotor 304, and described
One rotor 302 and the second rotor 303 are arranged on the pedestal 301, and the 3rd rotor 304 is arranged at the pedestal 301
One end, the rotating shaft of the rotor 303 of the first rotor 302 and second is perpendicular to horizontal plane, the shaft parallel of the 3rd rotor 304
In horizontal plane；
The electrical module 4 includes electrical enclosure, battery and control circuit 403, and the both ends of the electrical enclosure, which are provided with, opens
Mouthful, it is middle to be arranged at formed with electric accommodating cavity, the battery and the control circuit 403 in the electric accommodating cavity；
The operation module 5 includes operation cabin and investigation cabin 501, and the investigation cabin 501, which is arranged at below operation cabin, (to be made
It is with electrical enclosure to be connected one end above war cabin), ammunition accommodating cavity is provided with the operation cabin, for depositing ammunition load
503, the investigation cabin 501 is interior to be provided with camera 502, wherein, investigation bilge portion is provided with opening, and the camera lens of the camera passes through
The opening down bottom for being arranged at investigation cabin；
One end of the electrical enclosure of the electrical module 4 is connected with the other end of the pedestal 301 of power plant module 3, the electricity
The other end of gas shell is connected with the other end in the operation cabin of the operation module 5.
It was found from foregoing description, the beneficial effects of the present invention are：There is provided it is a kind of can with launching tube launch intelligence hang
Floating type ammunition, battlefield overhead is sent to using boost motor by intelligent floating type ammunition, is bowed using the investigation equipment of its carrying
Depending on investigating or performing military mission using the ammunition of its carrying, the difficulty that soldier assaults fortified position is substantially reduced, reduces casualty rate.
Implement example
In the present invention, rocket assist formula intelligence suspension bullet system also includes transmitter unit and earth station, it is necessary to front
Region is carried out investigations or during attack, and rocket assist formula intelligence suspension bullet is connected with earth station to code, after the completion of by rocket assist
Formula intelligence suspension bullet is launched by launching tube, and after the intelligence suspension of rocket assist formula bounces off exploitation shooting cylinder, boost motor is started working, point
Propellant is fired, intelligent suspension bullet is pushed to the overhead of target area, then boost motor separates with intelligent suspension bullet, and intelligence is outstanding
The electrical module work of floating bullet, carries out maneuvering flight, using the camera of operation module bottom to target area by power plant module
Domain carries out vertical view investigation, by the communication unit of the control circuit of electrical module, Image Real-time Transmission is returned into earth station, for operation
Person checks that operator can determine target of attack according to realtime graphic, and intelligent suspension bullet also possesses autonomous investigation, the function of attack,
Target of attack is voluntarily judged by plug-in, whole to be controlled without operator, earth station can control four pieces of rocket assists simultaneously
Formula intelligence suspension bullet；
The operation module of intelligent suspension bullet can be replaced other kinds of functional module, such as communication module, interference module
Deng.
Embodiment 1
First rotor 302 of the power plant module 3 of the intelligent suspension bullet is including the first propeller hub and the two panels being oppositely arranged just
To blade 305；
Second rotor 303 includes the second propeller hub and the reverse blade 306 of two panels being oppositely arranged；
3rd rotor 304 includes the 3rd propeller hub and the blade of two panels the 3rd being oppositely arranged.
First rotor 302, the second rotor 303 are used for the lifting and rotation of intelligent suspension bullet, and the 3rd rotor 304 is used to provide
Offset distance, make the body generation axle of intelligent suspension bullet inclined, and then obtain the ability advanced.
Embodiment 2
The positive blade 305 is articulated with the first propeller hub, and the positive blade 305 can be to the electric outer of the electrical module
Shell side is to rotation；The reversely blade 306 is articulated with the second propeller hub, and described reversely blade 306 can be to the electricity of the electrical module
Gas shell direction rotates；3rd blade is articulated with the 3rd propeller hub.
In the present embodiment, using the blade design of articulated structure, make blade folding storage, effectively reduce intelligent suspension
The volume of bullet, more conducively intelligent suspension bullet is launched using launching tube.
Embodiment 3
First rotor 302 of the power plant module 3 of the intelligent suspension bullet and the direction of rotation of the second rotor 303 are opposite.
In the present embodiment, mutually caused turn is offset between rotor using the first rotor and the second rotor of reverse rotation
Square, ensure the stability of intelligent suspension bullet flight.
Embodiment 4
The outside of the electrical enclosure of the electrical module 4 of the intelligent suspension bullet is provided with four raised lines 401, institute along its length
State raised line 401 and be provided with communication antenna.
In the present embodiment, in order to ensure the communication quality of intelligent suspension bullet, communication antenna is arranged at the outer of electrical enclosure
Side, while raised line also protects the blade in folded state.
Embodiment 5
The other end of the electrical enclosure of the electrical module 4 of the intelligent suspension bullet is provided with internal thread, the operation module 5
One end that operation cabin is connected with electrical enclosure is provided with the external screw thread of adaptation.
In the present embodiment, using being threadedly coupled between module, it is easy to the module disassembling, assembling and replacing of intelligent suspension bullet, helicitic texture
It is not limited to electrical enclosure and internal thread is set, and operation cabin sets the external screw thread of adaptation, vice versa.
Embodiment 6
The both ends of the assist device 1 of the boost motor are provided with opening, and the opening of one end of assist device 1 is connected with the first appearance
Chamber 101 is put, the opening of the other end is connected with the second accommodating cavity 102, wherein, the first accommodating cavity 101 is provided with ejection section, and second is accommodating
Chamber 102 is provided with separation unit, and the separation unit includes mobilizable top and moves back piston 104, and described push up moves back one end of piston 104 and be provided with and open
Mouthful, the piston accommodating cavity 105 of internal piston moves back on top in the opening UNICOM.
In the present embodiment, the assistant propellant for providing boost motor power is loaded in the first accommodating cavity of assist device, is led to
Overspray portion powder burning and produce boosting power, separation unit is provided with the second accommodating cavity of assist device, the top of separation unit is moved back
The other end of piston contacts with intelligent suspension bullet, and the piston accommodating cavity inside separation unit is provided with separator piston and promotes gunpowder, uses
Separating force is produced in blast, promotes piston forward, the disengaging movement of boost motor backward.
Embodiment 7
It is provided with the 3rd accommodating cavity 103 between two accommodating cavities of the assist device, the 3rd accommodating cavity 103 connection the
One accommodating cavity 101 and the second accommodating cavity 102.
In the present embodiment, it is provided with the 3rd accommodating cavity and delays gunpowder, after making assistant propellant burning totally, delays the several seconds
Ignite separation gunpowder again.
Embodiment 8
The outside of the assist device is provided with some wing plates along its length.
It is in 90 degree of outsides for being arranged at assist device between wing plate using four wing plates in the present embodiment, sets wing plate to have
Beneficial to the smooth flight of boost motor.
Embodiments of the invention are the foregoing is only, are not intended to limit the scope of the invention, it is every to utilize this hair
The equivalent structure or equivalent flow conversion that bright specification and accompanying drawing content are made, or directly or indirectly it is used in other related skills
Art field, is included within the scope of the present invention.
Claims (9)
- A kind of 1. rocket assist formula intelligence suspension bullet system, it is characterised in that：Including boost motor and intelligent suspension bullet, the boosting Device includes assist device and boost motor shell, and the assist device is arranged at one end of the boost motor shell, the boost motor The both ends of shell are provided with opening, and middle to play accommodating cavity formed with suspending, the intelligent suspension bullet is separably arranged at described help In the suspension bullet accommodating cavity of thruster shell；The intelligent suspension bullet includes power plant module, electrical module, operation module,The power plant module includes pedestal, the first rotor, the second rotor and the 3rd rotor, and first rotor and the second rotor are set It is placed on the pedestal, the 3rd rotor is arranged at one end of the pedestal, the rotating shaft of first rotor and the second rotor Perpendicular to horizontal plane, the shaft parallel of the 3rd rotor is in horizontal plane；The electrical module includes electrical enclosure, battery and control circuit, and the both ends of the electrical part shell are provided with opening, middle Formed with electric accommodating cavity, the battery and control circuit are arranged in the electric accommodating cavity；The operation module includes operation cabin and investigation cabin, and ammunition accommodating cavity is provided with the operation cabin, is set in the investigation cabin There is camera；The other end of one end of the electrical enclosure of the electrical module and the pedestal of power plant module connect, the electrical enclosure it is another One end is connected with the other end in the operation cabin of the operation module.
- 2. rocket assist formula intelligence suspension bullet system as claimed in claim 1, it is characterised in that：The intelligent suspension bullet moves First rotor of power module includes the first propeller hub and the two panels forward direction blade being oppositely arranged；Second rotor includes the second propeller hub and the reverse blade of two panels being oppositely arranged；3rd rotor includes the 3rd propeller hub and the blade of two panels the 3rd being oppositely arranged.
- 3. rocket assist formula intelligence suspension bullet system as claimed in claim 2, it is characterised in that：The positive blade is articulated with First propeller hub, the positive blade can rotate to the electrical enclosure direction of the electrical module；The reversely blade is articulated with the Two propeller hubs, the reversely blade can rotate to the electrical enclosure direction of the electrical module；3rd blade is articulated with the 3rd Propeller hub.
- 4. rocket assist formula intelligence suspension bullet system as claimed in claim 3, it is characterised in that：The intelligent suspension bullet moves The first rotor and the second rotor wing rotation of power module are in opposite direction.
- 5. rocket assist formula intelligence suspension bullet system as claimed in claim 4, it is characterised in that：The electricity of the intelligent suspension bullet The outside of the electrical enclosure of gas module is provided with four raised lines along its length, and the raised line is provided with communication antenna.
- 6. rocket assist formula intelligence suspension bullet system as claimed in claim 5, it is characterised in that：The electricity of the intelligent suspension bullet The other end of the electrical enclosure of gas module is provided with internal thread, and the one end in the operation cabin of the operation module is provided with the outer spiral shell of adaptation Line.
- 7. rocket assist formula intelligence suspension bullet system as claimed in any one of claims 1 to 6, it is characterised in that：The boosting The both ends of the assist device of device are provided with opening, and the opening of assist device one end is connected with the first accommodating cavity, and the opening of the other end connects The second accommodating cavity is connected to, wherein, the first accommodating cavity is provided with ejection section, and the second accommodating cavity is provided with separation unit, and the separation unit includes Move back piston on mobilizable top, and one end that piston is moved back on the top is provided with groove, and the other end is provided with opening, and work is moved back in top by the opening UNICOM Piston accommodating cavity inside plug.
- 8. rocket assist formula intelligence suspension bullet system as claimed in claim 7, it is characterised in that：Two of the assist device The 3rd accommodating cavity is provided between accommodating cavity, the 3rd accommodating cavity connects the first accommodating cavity and the second accommodating cavity.
- 9. rocket assist formula intelligence suspension bullet system as claimed in claim 8, it is characterised in that：The outside of the assist device Some wing plates are provided with along its length.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710170472.5A CN106839898B (en) | 2017-03-21 | 2017-03-21 | Rocket assist formula intelligence suspension bullet system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710170472.5A CN106839898B (en) | 2017-03-21 | 2017-03-21 | Rocket assist formula intelligence suspension bullet system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106839898A CN106839898A (en) | 2017-06-13 |
| CN106839898B true CN106839898B (en) | 2018-03-23 |
Family
ID=59130764
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710170472.5A Expired - Fee Related CN106839898B (en) | 2017-03-21 | 2017-03-21 | Rocket assist formula intelligence suspension bullet system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106839898B (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109373811B (en) * | 2018-09-27 | 2021-02-09 | 北京空间机电研究所 | Multi-stage actuating ejection device adopting follow-up charging |
| CN112429236B (en) * | 2020-12-10 | 2022-09-27 | 北京空间机电研究所 | Integrated investigation platform based on intercontinental missile carrying |
| CN112833717A (en) * | 2021-01-20 | 2021-05-25 | 航天科工微电子系统研究院有限公司 | Fusion type scouting and printing integrated aircraft layout system and method |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB681151A (en) * | 1948-05-31 | 1952-10-22 | Roger Aime Robert | Improvements in aircraft rocket-bomb launching devices |
| GB701960A (en) * | 1951-06-26 | 1954-01-06 | Bofors Ab | Improvements relating to suspension members for rockets |
| CN101249891A (en) * | 2007-12-29 | 2008-08-27 | 北京航空航天大学 | Rifle grenade type cartridge unmanned aircraft |
| CN202765289U (en) * | 2012-07-30 | 2013-03-06 | 江阴市公安局 | Multi-rotor police unmanned aerial vehicle |
| CN104139845B (en) * | 2014-07-30 | 2017-04-05 | 中国人民解放军空军工程大学 | Unmanned aerostat system |
| CN204433058U (en) * | 2015-01-22 | 2015-07-01 | 曹启武 | The full landform in low latitude collapsible scouting operation one unmanned plane |
| CN205345332U (en) * | 2016-01-22 | 2016-06-29 | 江苏数字鹰科技发展有限公司 | Police uses multi -functional unmanned aerial vehicle |
| CN206618342U (en) * | 2017-03-21 | 2017-11-07 | 深圳市轻准科技有限公司 | Rocket assist formula intelligence suspension bullet system |
-
2017
- 2017-03-21 CN CN201710170472.5A patent/CN106839898B/en not_active Expired - Fee Related
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| CN106839898A (en) | 2017-06-13 |
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Granted publication date: 20180323 |