CN206618342U - Rocket assist formula intelligence suspension bullet system - Google Patents
Rocket assist formula intelligence suspension bullet system Download PDFInfo
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- CN206618342U CN206618342U CN201720278162.0U CN201720278162U CN206618342U CN 206618342 U CN206618342 U CN 206618342U CN 201720278162 U CN201720278162 U CN 201720278162U CN 206618342 U CN206618342 U CN 206618342U
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- rotor
- accommodating cavity
- module
- suspension bullet
- intelligent suspension
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Abstract
The utility model provides a kind of intelligent suspension bullet system of rocket assist formula, including boost motor and intelligent suspension bullet, and 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 utility model 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, casualty rate is reduced.
Description
Technical field
The present invention relates to unmanned plane field, a kind of intelligent suspension bullet system of rocket assist formula 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 taken in time, cause attack it is invalid.
Scout after building or barrier target capability accordingly, it would be desirable to design a kind of can be provided for infantry and possess vertically
The floating type ammunition of striking capabilities.
Utility model content
Technical problem to be solved in the utility model is：There is provided a kind of infantry realized in short-distance and medium-distance street fighting investigation and
Possesses the ammunition outfit of vertical striking capabilities.
In order to solve the above-mentioned technical problem, the technical solution adopted in the utility model is：A kind of rocket assist formula is intelligently outstanding
Floating bullet system, including boost motor and intelligent suspension bullet, the boost motor include assist device and boost motor shell, the boosting dress
The one end for being placed in the boost motor shell is installed, the two ends of the boost motor shell are provided with opening, and centre is formed with suspension bullet appearance
Chamber is put, 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 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 being provided with ammunition accommodating cavity, the investigation cabin in operation cabin and investigation cabin, the operation cabin
It is interior to be provided with camera；
The other end connection of one end of the electrical enclosure of the electrical module and 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, the positive blade can to the electrical module electricity
Gas shell direction is rotated；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 is rotated；3rd blade is articulated with the 3rd propeller hub.
Further, the 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 is convex provided with four along its length
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
External screw thread of the one end in the operation cabin for module of fighting provided with 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
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 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 utility model are：A kind of intelligent floating type ammunition that can be launched with launching tube, profit are provided
Intelligent floating type ammunition is sent to battlefield overhead with boost motor, carries out overlooking investigation or utilization using the investigation equipment of its carrying
Its ammunition carried performs military mission, substantially reduces the difficulty that soldier assaults fortified position, reduces casualty rate.
Brief description of the drawings
Concrete structure of the present utility model is described in detail below in conjunction with the accompanying drawings：
Fig. 1 is the structural representation of the intelligent suspension bullet system of rocket assist formula of the present utility model；
Fig. 2 is the structural representation of the assist device of the intelligent suspension bullet system of rocket assist formula of the present utility model；
Fig. 3 is the structural representation of the power plant module of the intelligent suspension bullet system of rocket assist formula of the present utility model；
Fig. 4 is the structural representation of the electrical module of the intelligent suspension bullet system of rocket assist formula of the present utility model；
Fig. 5 is the structural representation of the operation module of the intelligent suspension bullet system of rocket assist formula of the present utility model；
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.
Embodiment
To describe technology contents of the present utility model, construction feature, the objects and the effects in detail, below in conjunction with implementation
Mode simultaneously coordinates accompanying drawing to be explained in detail.
Fig. 1 is referred to Fig. 5, a kind of intelligent suspension bullet system of rocket assist formula, 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 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, 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 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 two ends of the electrical enclosure, which are provided with, opens
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, which is arranged at below operation cabin, (to be made
To be connected one end with electrical enclosure above war cabin), provided with ammunition accommodating cavity in 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 is down
The bottom in investigation cabin is arranged at through opening；
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 utility model are：A kind of intelligence that can be launched with launching tube is provided
Energy floating type ammunition, battlefield overhead is sent to using boost motor by intelligent floating type ammunition, and investigation equipment using its carrying is entered
Row overlooks investigation or performs military mission using the ammunition of its carrying, substantially reduces the difficulty that soldier assaults fortified position, reduces injures and deaths
Rate.
Implement example
In the utility model, rocket assist formula intelligence suspension bullet system also includes transmitter unit and earth station, it is necessary to right
Front region is carried out investigations or during attack, and the intelligent suspension bullet of rocket assist formula is connected with earth station to code, after the completion of by rocket
Assisted intelligence suspension bullet is launched by launching tube, and rocket assist formula, which intelligently suspends, to be bounced off after exploitation shooting cylinder, and boost motor starts work
Make, light propellant, intelligent suspension bullet is pushed to the overhead of target area, then boost motor is separated with intelligent suspension bullet,
The electrical module work of intelligent suspension bullet, carries out maneuvering flight by power plant module, utilizes the camera pair of operation module bottom
Target area carries out vertical view investigation, and by the communication unit of the control circuit of electrical module, Image Real-time Transmission is returned into earth station,
Checked for operator, operator can determine target of attack according to realtime graphic, intelligent suspension bullet also possesses autonomous investigation, attack
Function, voluntarily judges target of attack, whole without operator's control, earth station can control four pieces of rockets simultaneously by plug-in
Assisted 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, 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, the reverse blade 306 can to the electrical module electricity
Gas shell direction is rotated；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 conducive to launch 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, turn mutually produced between rotor is offset using the first rotor and the second rotor of reverse rotation
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 along its length provided with four raised lines 401, institute
Raised line 401 is stated 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
External screw thread of the one end that operation cabin is connected with electrical enclosure provided with 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 mobilizable top and moves back piston 104, and described push up moves back one end of piston 104 provided with opening
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, in the second accommodating cavity of assist device be provided with separation unit, 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 promotes gunpowder provided with separator piston, is used
Separating force is produced in blast, piston is promoted 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, is made after assistant propellant burning totally, delay 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.
Embodiment of the present utility model is the foregoing is only, the scope of the claims of the present utility model is not thereby limited, it is every
The equivalent structure or equivalent flow conversion made using the utility model specification and accompanying drawing content, or be directly or indirectly used in
Other related technical fields, are similarly included in scope of patent protection of the present utility model.
Claims (9)
1. a kind of intelligent suspension bullet system of rocket assist formula, 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 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 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, which includes being provided with ammunition accommodating cavity, the investigation cabin in operation cabin and investigation cabin, the operation cabin, to be set
There is camera；
One end of the electrical enclosure of the electrical module and the pedestal of power plant module the other end connection, the electrical enclosure it is another
One end is connected with the other end in the operation cabin of the operation module.
2. the intelligent suspension bullet system of rocket assist formula as claimed in claim 1, it is characterised in that：The intelligent suspension bullet it is dynamic
First rotor of power module includes the first propeller hub and the positive blade of the two panels 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. the intelligent suspension bullet system of rocket assist formula as claimed in claim 2, 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. the intelligent suspension bullet system of rocket assist formula as claimed in claim 3, it is characterised in that：The intelligent suspension bullet it is dynamic
The first rotor and the second rotor wing rotation of power module are in opposite direction.
5. the intelligent suspension bullet system of rocket assist formula 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 along its length provided with four raised lines, and the raised line is provided with communication antenna.
6. the intelligent suspension bullet system of rocket assist formula 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, the outer spiral shell of the one end provided with adaptation in the operation cabin of the operation module
Line.
7. the intelligent suspension bullet system of rocket assist formula 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 on the opening UNICOM top
Piston accommodating cavity inside plug.
8. the intelligent suspension bullet system of rocket assist formula 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. the intelligent suspension bullet system of rocket assist formula 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 |
|---|---|---|---|
| CN201720278162.0U CN206618342U (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 |
|---|---|---|---|
| CN201720278162.0U CN206618342U (en) | 2017-03-21 | 2017-03-21 | Rocket assist formula intelligence suspension bullet system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206618342U true CN206618342U (en) | 2017-11-07 |
Family
ID=60233286
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720278162.0U Withdrawn - After Issue CN206618342U (en) | 2017-03-21 | 2017-03-21 | Rocket assist formula intelligence suspension bullet system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206618342U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106839898A (en) * | 2017-03-21 | 2017-06-13 | 深圳市轻准科技有限公司 | Rocket assist formula intelligence suspension bullet system |
| CN108195235A (en) * | 2017-12-29 | 2018-06-22 | 广州卫富科技开发有限公司 | A kind of micro-sound video detecting bullet |
-
2017
- 2017-03-21 CN CN201720278162.0U patent/CN206618342U/en not_active Withdrawn - After Issue
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106839898A (en) * | 2017-03-21 | 2017-06-13 | 深圳市轻准科技有限公司 | Rocket assist formula intelligence suspension bullet system |
| CN108195235A (en) * | 2017-12-29 | 2018-06-22 | 广州卫富科技开发有限公司 | A kind of micro-sound video detecting bullet |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20171107 Effective date of abandoning: 20180323 |