CN106839898A - Rocket assist formula intelligence suspension bullet system - Google Patents
Rocket assist formula intelligence suspension bullet system Download PDFInfo
- Publication number
- CN106839898A CN106839898A CN201710170472.5A CN201710170472A CN106839898A CN 106839898 A CN106839898 A CN 106839898A CN 201710170472 A CN201710170472 A CN 201710170472A CN 106839898 A CN106839898 A CN 106839898A
- Authority
- CN
- China
- Prior art keywords
- rotor
- accommodating cavity
- module
- suspension bullet
- 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.)
- Granted
Links
- 239000000725 suspension Substances 0.000 title claims abstract description 66
- 238000011835 investigation Methods 0.000 claims abstract description 19
- 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
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000000151 deposition Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000000034 method Methods 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 includes 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 that reversely rotate each other, and responsible offset distance the 3rd rotor；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 or the ammunition execution military mission using its carrying using its investigation equipment for carrying, the difficulty that soldier assaults fortified position is substantially reduced, casualty rate is reduced.
Description
Technical field
The present invention relates to unmanned plane field, a kind of rocket assist formula intelligence suspension bullet system is referred in particular to.
Background technology
In modern war, infantry's street fighting used when fighting it is straight take aim at ammunition, with the hang time is short, Map and image database is difficult
Shortcoming, and easily stick one's chin out, thus according to needs, unmanned plane accessory system is occurred in that, but existing individual soldier patrols winged weapon
Substantially Fixed Wing AirVehicle, it is desirable to have certain speed can just be stayed in the air, it is impossible to hovering on one point, during to target observations only
Energy circuit, the investigation ability for narrow and small street lane is extremely limited.And when striking target, unmanned plane also needs to make larger
Maneuver, easily cause enemy to note, workaround is taken in time, cause attack it is invalid.
Accordingly, it would be desirable to design and a kind of can scout after building or barrier target capability and possess vertically for infantry provides
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 investigating and possessing in short-distance and medium-distance street fighting
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 sets
One end of the boost motor shell is placed in, the two ends of the boost motor shell are provided with opening, and centre is formed with suspension and plays accommodating cavity,
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
Perpendicular to horizontal plane, the shaft parallel of the 3rd rotor is in horizontal plane for rotating shaft；
The electrical module includes electrical enclosure, battery and control circuit, and the two ends of the electrical part shell are provided with opening,
Centre is formed with electric accommodating cavity, and 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, the investigation cabin are provided with the operation cabin
Inside it is provided with camera；
One end of the electrical enclosure of the electrical module is connected with the other end of the pedestal of power plant module, 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 reverse blade is articulated with the second propeller hub, and the reverse blade can be to the electric of the electrical module
Shell direction rotates；3rd blade is articulated with the 3rd propeller hub.
Further, first rotor and the second rotor wing rotation of the power plant module of the intelligent suspension bullet are in opposite direction.
Further, the outside of the electrical enclosure of the electrical module of the intelligent suspension bullet be provided with along its length four it is convex
Bar, the raised line is 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 of module of fighting is provided with the external screw thread of adaptation.
Further, the two 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 is connected with the second accommodating cavity, wherein, the first accommodating cavity is provided with ejection section, the second accommodating cavity
Separation unit is provided with, the separation unit includes that piston is moved back on mobilizable top, and one end that piston is moved back on the top is provided with groove, and the other end sets
There is opening, the piston accommodating cavity of internal piston is moved back on the opening UNICOM top.
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 its investigation equipment for carrying or is taken using it
The ammunition of band performs military mission, substantially reduces the difficulty that soldier assaults fortified position, and reduces casualty rate.
Brief description of the drawings
Concrete structure of the invention is described in detail in detail below in conjunction with the accompanying drawings：
Fig. 1 is the structural representation of rocket assist formula intelligence suspension bullet system of the invention；
Fig. 2 is the structural representation of the assist device of rocket assist formula intelligence suspension bullet system of the invention；
Fig. 3 is the structural representation of the power plant module of rocket assist formula intelligence suspension bullet system of the invention；
Fig. 4 is the structural representation of the electrical module of rocket assist formula intelligence suspension bullet system of the invention；
Fig. 5 is the structural representation of the operation module of rocket assist formula intelligence suspension bullet system of the 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- controls circuit；
5- operation modules；501- investigates equipment；502- cameras；503- ammunition load.
Specific embodiment
To describe technology contents of the invention, structural feature, the objects and the effects in detail, below in conjunction with implementation method
And coordinate accompanying drawing 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 two ends of the boost motor shell 2 are provided with opening, and centre is formed with suspension and plays accommodating cavity, and the intelligent suspension bullet separably sets
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, described the
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 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 two ends of the electrical enclosure are provided with out
Mouthful, centre is formed with electric accommodating cavity, and the battery and the control circuit 403 are arranged in the electric accommodating cavity；
The operation module 5 includes operation cabin and investigation cabin 501, and the investigation cabin 501 is arranged at below operation cabin (to be made
War is to be connected one end with electrical enclosure above cabin), ammunition accommodating cavity is provided with the operation cabin, for depositing ammunition load
503, camera 502 is provided with the investigation cabin 501, wherein, investigation bilge portion is provided with opening, and the camera lens of the camera is passed 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.
Knowable to foregoing description, the beneficial effects of the present invention are：A kind of intelligence that can be launched with launching tube is provided to hang
Floating type ammunition, battlefield overhead is sent to using boost motor by intelligent floating type ammunition, is bowed using its investigation equipment for carrying
Depending on investigating or using the ammunition execution military mission of its carrying, substantially reducing the difficulty that soldier assaults fortified position, casualty rate is reduced.
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 rocket assist formula is intelligently suspended after bouncing off exploitation shooting cylinder, and boost motor is started working, point
Combustion propellant, intelligent suspension bullet is pushed to the overhead of target area, and then boost motor is separated 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 without operator's control, 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 includes the first propeller hub with 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, makes the body of intelligent suspension bullet produce axle partially, 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 reverse blade 306 is articulated with the second propeller hub, and the reverse 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, is more conducively launched intelligent suspension bullet 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, using reversely rotate the first rotor and the second rotor to offset rotor between mutually produce turn
Square, it is ensured that 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 threaded connection 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 two 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 houses
Chamber 102 is provided with separation unit, and the separation unit includes that piston 104 is moved back on mobilizable top, and one end that piston 104 is moved back on the top is provided with out
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, 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 is contacted with intelligent suspension bullet, and the piston accommodating cavity inside separation unit is provided with separator piston and promotes gunpowder, is used
Separating force is produced in blast, piston is promoted forward, boost motor disengaging movement backward.
Embodiment 7
It is provided with the 3rd accommodating cavity 103 between two accommodating cavities of the assist device, the connection of the 3rd accommodating cavity 103 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 assistant propellant is burnt 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.
In the present embodiment, using four wing plates, the outside for being arranged at assist device in 90 degree between wing plate, setting wing plate has
Beneficial to the smooth flight of boost motor.
Embodiments of the invention are the foregoing is only, the scope of the claims of the invention is not thereby limited, it is every to utilize this hair
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)
1. a kind of 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 two ends of shell are provided with opening, and centre is formed with suspension and plays accommodating cavity, and the intelligent suspension bullet is separably arranged at described helping
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 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 two ends of the electrical part shell are provided with opening, middle
Electric accommodating cavity is formed with, 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；
One end of the electrical enclosure of the electrical module is connected with the other end of the pedestal of power plant module, 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 as claimed in claim 1 intelligence suspension bullet system, it is characterised in that：The intelligent suspension bullet it is dynamic
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 as claimed in claim 2 intelligence suspension bullet system, it is characterised in that：The positive blade is articulated with
First propeller hub, the positive blade can be rotated to the electrical enclosure direction of the electrical module；The reverse blade is articulated with
Two propeller hubs, the reverse blade can be rotated to the electrical enclosure direction of the electrical module；3rd blade is articulated with the 3rd
Propeller hub.
4. rocket assist formula as claimed in claim 3 intelligence suspension bullet system, it is characterised in that：The intelligent suspension bullet it is dynamic
First rotor and the second rotor wing rotation of power module are in opposite direction.
5. rocket assist formula as claimed in claim 4 intelligence suspension bullet system, 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 as claimed in claim 5 intelligence suspension bullet system, 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 two 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 as claimed in claim 7 intelligence suspension bullet system, 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 as claimed in claim 8 intelligence suspension bullet system, 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 true CN106839898A (en) | 2017-06-13 |
| CN106839898B 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) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109373811A (en) * | 2018-09-27 | 2019-02-22 | 北京空间机电研究所 | A kind of multistage actuation catapult-launching gear using travelling charge |
| CN112429236A (en) * | 2020-12-10 | 2021-03-02 | 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 |
Citations (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 |
| CN104139845A (en) * | 2014-07-30 | 2014-11-12 | 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
Patent Citations (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 |
| CN104139845A (en) * | 2014-07-30 | 2014-11-12 | 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 |
Non-Patent Citations (2)
| Title |
|---|
| 胡西博: ""悬浮子弹药悬停技术研究"", 《中国优秀硕士学位论文全文数据库 工程科技Ⅱ辑》 * |
| 苏京昭 等: ""悬浮弹旋翼结构参数对其气动力的影响分析"", 《兵工自动化》 * |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109373811A (en) * | 2018-09-27 | 2019-02-22 | 北京空间机电研究所 | A kind of multistage actuation catapult-launching gear using travelling charge |
| 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 |
| CN112429236A (en) * | 2020-12-10 | 2021-03-02 | 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 |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106839898B (en) | 2018-03-23 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN109436296B (en) | Barrel-type launching folding wing unmanned aerial vehicle and launching method thereof | |
| CN103101621B (en) | Parafoil aircraft applicable to cylindrical space loading | |
| CN103043214A (en) | Folding type unmanned plane | |
| CN106839898B (en) | Rocket assist formula intelligence suspension bullet system | |
| CN110065634A (en) | Unmanned flight robot based on the cold power-assisted transmitting of compressed gas | |
| CN108750101A (en) | A kind of super maneuver high speed compound unmanned rotary wing aircraft, assembly, assembly and disassembly methods | |
| CN108482635A (en) | Inflator wing type aircraft capable of being parked | |
| CN206618342U (en) | Rocket assist formula intelligence suspension bullet system | |
| CN211626280U (en) | Four-duct propelling type small missile | |
| CN103968714A (en) | Defending bomb device hung in air | |
| CN110371283B (en) | Intelligent flexible inflatable wing unmanned aerial vehicle structure | |
| CN203020540U (en) | Folding unmanned aerial vehicle | |
| CN113371182A (en) | Barrel-type transmitted reconnaissance attack rotor unmanned aerial vehicle | |
| CN108032309A (en) | Low detectivity air defense robot | |
| CN104503458A (en) | Micro individual combat unmanned plane system | |
| CN109515732B (en) | Combined aircraft based on barrel type launching | |
| CN116353855A (en) | Photoelectric hybrid power multipurpose fire-fighting unmanned aerial vehicle | |
| CN110940236B (en) | Non-aiming intelligent patrol projectile | |
| CN211346558U (en) | Miniature rocket bomb | |
| CN110595293B (en) | Working method of fixed wing-rotor wing composite unmanned aerial vehicle | |
| CN110567326B (en) | Fixed wing-rotor wing composite unmanned aerial vehicle | |
| CN214792811U (en) | Flying projectile body structure is patrolled to whole compression molding carbon-fibre composite | |
| CN110763090B (en) | Combinable and deformable primary-secondary type patrol and play integrated flying bomb and working method thereof | |
| CN104121827B (en) | A kind of stealthy bombing guided missile of repeatable utilization | |
| CN109323633B (en) | Single-soldier hand-thrown type fly-round projectile with conventional layout |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180323 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |