CN108931164A - A kind of turn emitter - Google Patents
A kind of turn emitter Download PDFInfo
- Publication number
- CN108931164A CN108931164A CN201810647632.5A CN201810647632A CN108931164A CN 108931164 A CN108931164 A CN 108931164A CN 201810647632 A CN201810647632 A CN 201810647632A CN 108931164 A CN108931164 A CN 108931164A
- Authority
- CN
- China
- Prior art keywords
- emitting head
- thermally conductive
- power house
- motive force
- emitter
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- 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.)
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B30/00—Projectiles or missiles, not otherwise provided for, characterised by the ammunition class or type, e.g. by the launching apparatus or weapon used
- F42B30/02—Bullets
-
- 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
- F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
- F42B10/38—Range-increasing arrangements
- F42B10/42—Streamlined projectiles
-
- 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
- F42B10/60—Steering arrangements
- F42B10/66—Steering by varying intensity or direction of thrust
-
- 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
Abstract
A kind of turn emitter provided by the invention, comprising: emitter ontology is equipped with first order kinetics medium in inner cavity；Emitting head, the front end of the emitter ontology is set, it is equipped with thermal insulation layer between the emitting head and the emitter ontology, second motive force medium is equipped in the inner cavity of the emitting head and for receiving excitation control instruction to excite the excitation structure of the second motive force medium；The emitting head circumferential direction is equipped at least one injection channel, and one end of the injection channel is connected to the second motive force medium, and the other end is penetrated through to the injection channel of the emitting head lateral outer.Solve the problems, such as that emitter in the prior art is easily blocked object and blocks and reduce strike accuracy.
Description
Technical field
The invention belongs to emitter technical fields, a kind of emitter suitable for non-rotating advance, and in particular to turn
Emitter.
Background technique
Emitter in the prior art mainly includes shell case and bullet, and when pulling trigger, bullet is excited de- with shell case
From and from projected in bore, with the object that strikes target.If emitter is launched from bore there are shelter in front of object
After going, since bullet is run only along a direction, it is easily blocked object and blocks, speed reduces rapidly out of service, it is difficult to
It passes through shelter and precision strike is carried out to object, reduce strike accuracy.
In order to solve the above-mentioned technical problem, 105498254 A of Chinese patent literature CN discloses a kind of emitter, such as Fig. 6
It is shown comprising: body 101；Warhead-containing body 102, the channel 103 with open rearward end；The bullet 102 includes bullet seat
104 and bullet nut cap 105, the front end of the bullet seat 104 be provided with installation cavity, the bullet nut cap 105 is threaded in bullet
In the installation cavity of headstock 104, the channel 103 is arranged on the bullet seat 104 and is connected to the installation cavity；Activity
Block 106 is provided with the cavity 105 being connected to the channel 103；Driving device 107, including drive seat 108 and drive rod 109,
The drive seat 108 is movably connected in the side of the movable block 106, and the rear end of the drive rod 109 is fixed on the driving
On seat 108, front end passes through the cavity 105 and extend into the channel 103, and cannot be to hair by the channel 103 limitation
The rear end of beam is mobile；After the transmitting of above-mentioned warhead-containing body, after movable block unlock, drive seat and drive rod under the action of inertia,
It can still be run along channel forward end, so that the front-end driven bullet cut-through object by drive rod is run forwards, from
And carry out Secondary Emission.
But bullet can not accurately bypass shelter, simply by effect of inertia avoiding obstacles to shelter
The target at rear is hit, and bullet hit precision is lower, can not be flown along estimated camber line, it may appear that can not successfully hide
The problem of shelter, causes bullet that can not hit the mark.
Summary of the invention
Therefore, it is blocked the technical problem to be solved in the present invention is that emitter in the prior art is overcome to be easily blocked object
And reduce the technological deficiency of strike accuracy.
For this purpose, the present invention provides a kind of turn emitter, including
Emitter ontology is equipped with first order kinetics medium in inner cavity；
Emitting head, the emitting head are non-rotary bullet in flight course, and the front end of the emitter ontology is arranged in,
Thermal insulation layer is equipped between the emitting head and the emitter ontology, be equipped in the inner cavity of the emitting head second motive force medium and
For receiving excitation control instruction to excite the excitation structure of the second motive force medium；
The emitting head circumferential direction is equipped at least one injection channel, one end connection described two of the injection channel
Grade dynamic medium, the other end are penetrated through to the injection channel of the emitting head lateral outer.
The excitation structure includes: the double gold plaques being mounted in the emitting head inner cavity, thermally conductive excitation bar and accommodates
State the power house of second motive force medium；The thermally conductive excitation bar and double gold plaques are arranged on the power house, and described dynamic
Power room is equipped with the splicing structure being detachably connected with the bullet shell of the emitting head；
Described thermally conductive excitation bar one end connects the second motive force medium, and the other end is oppositely arranged with double gold plaques, institute
It states and is equipped with gap between double gold plaques and the thermally conductive excitation bar, double gold plaque temperature distortions are connected with the thermally conductive excitation bar.
The bottom of the emitting head is equipped with the installing port for installing the excitation structure.
The power house is arranged at the installing port, and the emitting head of sealing structure is surrounded with the bullet shell.
The splicing structure includes being separately positioned on the edge and the power house of the installing port, mutual cooperation phase
Helicitic texture even.
The emitting head is made of metal material；The power house is made of heat insulator.
The thermally conductive excitation bar protrudes into the power house outside the power house and connect with the second motive force medium.
The power house upper end is equipped with the accommodation groove for being embedded in the thermally conductive excitation bar, the accommodation groove and double gold
Piece surrounds the accommodation chamber for accommodating the thermally conductive excitation bar.
The accommodation groove is equipped with the extension channel extended towards the injection channel, and the lower end for extending channel is equipped with
Opening, the thermally conductive excitation bar pass through the opening and are connected with the second motive force medium.
The second motive force medium is propellant powder, is filled with sealing wax in the injection channel.
The emitter is bullet.
Technical solution of the present invention has the advantages that
1. turn emitter provided by the invention, including emitting head and inner cavity are equipped with first order kinetics medium emission body sheet
Body is equipped with thermal insulation layer between emitting head and emitter ontology, second motive force medium is equipped in the inner cavity of emitting head and for receiving
Control instruction is excited to excite the excitation structure of the second motive force medium.When the pistol for being provided with controller sends excitation control
It instructs to excitation structure, excitation structure lights second motive force medium to push emitting head to turn round.To enable emitting head to bypass
Shelter realizes that the object at shelter rear is hit in bullet turn to hit the target at shelter rear,
Effectively improve bullet shooting precision.
2. turn emitter provided by the invention, the excitation structure include: the double gold plaques being mounted in emitting head inner cavity,
Thermally conductive excitation bar and the power house for being equipped with second motive force medium；Thermally conductive excitation bar one end connects second motive force medium, the other end
It is oppositely arranged with double gold plaques, gap, double gold plaque temperature distortions, with thermally conductive excitation bar phase is equipped between double gold plaques and thermally conductive excitation bar
Even.When emitting head in-flight, double gold plaques are because overcome air drag temperature to gradually rise generation temperature distortion, with thermally conductive excitation bar
It is connected, thermally conductive excitation bar transfers heat to second motive force medium, pushes emitting head to turn round to light second motive force medium.?
The dynamic medium that thermally conductive excitation bar can just ignite in bullet after emitting head flight a period of time, it is double that user can according to need replacement
Gold plaque, thermally conductive excitation bar thermal conductivity or change second motive force medium number to change turn time and the turn of emitting head
Amplitude, to carry out precision strike to target around shelter.
3. turn emitter provided by the invention, the bottom of emitting head, and the bottom of bullet shell is arranged in installing port
It is made of power house, installs the power house of double gold plaques and thermally conductive excitation bar, can be convenient, be quickly connected with bullet shell,
The improper installation for improving emitter, difficulty of processing will not be selected because of the position of installing port.
4. turn emitter provided by the invention, power house upper end is equipped with the accommodation groove for being embedded in thermally conductive excitation bar, holds
It sets slot and double gold plaques surrounds the accommodation chamber for accommodating thermally conductive excitation bar.Accommodation chamber can effectively completely cut off in emitting head flight course gram
Heat caused by air drag is taken, it, just can be by heat after being connected with thermally conductive excitation bar only when double gold plaques continue temperature distortion
Thermally conductive excitation bar is passed to, the opening that thermally conductive excitation bar is then passed through accommodating trench bottom lights second motive force medium.Accommodation chamber can be with
Play the role of the thermally conductive excitation bar of isolation, thermally conductive excitation bar is avoided voluntarily to excite second motive force medium.
5. turn emitter provided by the invention, it is logical that the slot bottom of accommodation groove is additionally provided with the extension extended towards injection channel
Road extends channel lower end and is equipped with opening, and thermally conductive excitation bar passes through opening and is connected with propellant powder.Excitation bar extends to bullet bottom
It is connected again with the indoor propellant powder of power after injection channel, avoids power house top and first ignite and drive the transmitting of bullet bottom end again
The phenomenon that efficacy-enhancing ingredient fires is conducive to improve effect of igniting to reduce the risk of bad bullet, improves dynamic medium and pushes away to bullet turn
Movement is used.
Detailed description of the invention
It, below will be to specific in order to illustrate more clearly of the specific embodiment of the invention or technical solution in the prior art
Embodiment or attached drawing needed to be used in the description of the prior art be briefly described, it should be apparent that, it is described below
Attached drawing is some embodiments of the present invention, for those of ordinary skill in the art, before not making the creative labor
It puts, is also possible to obtain other drawings based on these drawings.
Fig. 1 is the structural schematic diagram of emitter provided by the invention；
Fig. 2 is the structural schematic diagram of emitting head provided by the invention；
Fig. 3 is the structural schematic diagram of power house provided by the invention；
Fig. 4 is the structural schematic diagram of bullet shell provided by the invention；
Fig. 5 is the structural schematic diagram of thermally conductive excitation bar provided by the invention；
Fig. 6 is the structural schematic diagram of turn bullet in the prior art.
Description of symbols:
1- emitter ontology；2- first order kinetics medium；3- emitting head；4- thermal insulation layer；5- second motive force medium；6- injection is logical
Road；7- bullet shell；The bis- gold plaques of 8-；The thermally conductive excitation bar of 9-；10- power house；11- installing port；12- accommodation groove；13- extends logical
Road；14- opening；101- body；102- warhead-containing body；The channel 103-；104- bullet seat；105- bullet nut cap；106- movable block；
107- driving device；108- drive seat；109- drive rod
Specific embodiment
Technical solution of the present invention is clearly and completely described below in conjunction with attached drawing, it is clear that described implementation
Example is a part of the embodiment of the present invention, instead of all the embodiments.Based on the embodiments of the present invention, ordinary skill
Personnel's every other embodiment obtained without making creative work, shall fall within the protection scope of the present invention.
In the description of the present invention, it should be noted that term " front end " " rear end " refers to the front of the bullet direction of the launch
The rear and.
Embodiment 1
If the emitter of Fig. 1 is bullet comprising:
Emitter ontology 1 is equipped with first order kinetics medium 2 in inner cavity；
The front end of emitter ontology 1, emitting head 3 and emitter ontology 1 is arranged in emitting head 3 made of metal
Between be equipped with thermal insulation layer 4, propellant powder is equipped in the inner cavity of emitting head 3 and excites control instruction with excitation-emission medicine for receiving
Excitation structure；
3 circumferential direction of emitting head is equipped with an injection channel 6, sealing wax is filled in injection channel 6, and one end connects
Logical propellant powder, the other end are penetrated through to the injection channel 6 of 3 lateral outer of emitting head.When the pistol for being provided with controller sends excitation
For control instruction to excitation structure, excitation structure lights propellant powder to push emitting head to turn round.To enable emitting head around screening
Block material is realized that the object at shelter rear is hit in bullet turn, is had to hit the target at shelter rear
Improve bullet shooting precision in effect ground.
In the present embodiment, as the excitation structure of Fig. 2 includes: the double gold plaques 8 being mounted in 3 inner cavity of emitting head, thermally conductive
Excitation bar 9 and the power house 10 for being equipped with propellant powder；Thermally conductive excitation bar 9 and double gold plaques 8 are arranged made of heat insulator
On power house 10, and power house 10 is equipped with the helicitic texture being detachably connected with the bullet shell 7 of emitting head 3；Such as the hair of Fig. 4
Penetrate first 3 bottom and be equipped with installing port 11 for installing excitation structure, helicitic texture be separately positioned on installing port 11 edge and
On power house 10, power house 10 surrounds the emitting head 3 of sealing structure with bullet shell 7.The bottom of emitting head is arranged in installing port,
And the bottom of bullet shell is made of power house, is installed the power house of double gold plaques and thermally conductive excitation bar, be can be convenient, fast
Ground is connected with bullet shell, and the improper installation for improving emitter, difficulty of processing will not be selected because of the position of installing port.
Thermally conductive 9 one end of excitation bar connects propellant powder, and the other end is oppositely arranged with double gold plaques 8, double gold plaques 8 and thermally conductive excitation bar
Gap is equipped between 9, double 8 temperature distortions of gold plaque are connected with thermally conductive excitation bar 9.When emitting head in-flight, double gold plaques are because overcome
Air drag temperature gradually rises generation temperature distortion, is connected with thermally conductive excitation bar, and thermally conductive excitation bar transfers heat to transmitting
Medicine pushes emitting head to turn round to light propellant powder.Thermally conductive excitation bar can just ignite bullet after emitting head flight a period of time
Interior dynamic medium, user can according to need replace double gold plaques, thermally conductive excitation bar thermal conductivity or change propellant powder number
To change turn time and the turn amplitude of emitting head, to carry out precision strike to target around shelter.
In the present embodiment, as 10 upper end of power house of Fig. 3 and Fig. 5 is equipped with the accommodating for being embedded in thermally conductive excitation bar 9
Slot 12, accommodation groove 12 and double gold plaques 8 surround the accommodation chamber for accommodating thermally conductive excitation bar 9.Accommodation chamber can effectively completely cut off emitting head
Overcome heat caused by air drag in flight course, only when double gold plaques continue temperature distortion, is connected with thermally conductive excitation bar
Afterwards, thermally conductive excitation bar can be just transferred heat to, the opening that thermally conductive excitation bar is then passed through accommodating trench bottom lights propellant powder.Accommodating
Room can play the role of the thermally conductive excitation bar of isolation, avoid thermally conductive excitation bar voluntarily excitation-emission medicine.
Accommodation groove 12 is equipped with the extension channel 13 extended towards injection channel 6, and the lower end for extending channel 13 is equipped with opening
14, thermally conductive excitation bar 9 passes through opening 14 and is connected with propellant powder.To make thermally conductive excitation bar 9 protrude into power outside power house 10
It is connect behind room 10 with propellant powder.It is connected again with the indoor propellant powder of power after exciting bar to extend to the injection channel of bullet bottom,
Avoid power house top the phenomenon that driving the propellant powder of bullet bottom end to ignite again of first igniting has to reduce the risk of bad bullet
It ignites effect conducive to raising, improves the impetus that dynamic medium turns round to bullet.
Embodiment 2
Emitter is bullet comprising:
Emitter ontology 1 is equipped with first order kinetics medium 2 in inner cavity；
The front end of emitter ontology 1, emitting head 3 and emitter ontology 1 is arranged in emitting head 3 made of metal
Between be equipped with thermal insulation layer 4, propellant powder is equipped in the inner cavity of emitting head 3 and excites control instruction with excitation-emission medicine for receiving
Excitation structure；
3 circumferential direction of emitting head is equipped with an injection channel 6, sealing wax is filled in injection channel 6, and one end connects
Logical propellant powder, the other end are penetrated through to the injection channel 6 of 3 lateral outer of emitting head.When the pistol for being provided with controller sends excitation
For control instruction to excitation structure, excitation structure lights propellant powder to push emitting head to turn round.To enable emitting head around screening
Block material is realized that the object at shelter rear is hit in bullet turn, is had to hit the target at shelter rear
Improve bullet shooting precision in effect ground.
In the present embodiment, excitation structure includes: the double gold plaques 8 being mounted in 3 inner cavity of emitting head, thermally conductive excitation bar 9
With the power house 10 for being equipped with propellant powder；Thermally conductive excitation bar 9 and double gold plaques 8 are arranged in power house 10 made of heat insulator
On, and power house 10 is equipped with the helicitic texture being detachably connected with the bullet shell 7 of emitting head 3；3 bottom of emitting head, which is equipped with, to be used
In the installing port 11 of installation excitation structure, helicitic texture is separately positioned on the edge and power house 10 of installing port 11, power
Room 10 and bullet shell 7 surround the emitting head 3 of sealing structure.Installing port is arranged in the bottom of emitting head, and bullet shell
Bottom is made of power house, installs the power house of double gold plaques and thermally conductive excitation bar, can be convenient, quickly with shell phase outside bullet
Even, the improper installation for improving emitter, difficulty of processing will not be selected because of the position of installing port.
Thermally conductive 9 one end of excitation bar connects propellant powder, and the other end is oppositely arranged with double gold plaques 8, double gold plaques 8 and thermally conductive excitation bar
Gap is equipped between 9, double 8 temperature distortions of gold plaque are connected with thermally conductive excitation bar 9.When emitting head in-flight, double gold plaques are because overcome
Air drag temperature gradually rises generation temperature distortion, is connected with thermally conductive excitation bar, and thermally conductive excitation bar transfers heat to transmitting
Medicine pushes emitting head to turn round to light propellant powder.Thermally conductive excitation bar can just ignite bullet after emitting head flight a period of time
Interior dynamic medium, user can according to need replace double gold plaques, thermally conductive excitation bar thermal conductivity or change propellant powder number
To change turn time and the turn amplitude of emitting head, to carry out precision strike to target around shelter.
Obviously, the above embodiments are merely examples for clarifying the description, and does not limit the embodiments.It is right
For those of ordinary skill in the art, can also make on the basis of the above description it is other it is various forms of variation or
It changes.There is no necessity and possibility to exhaust all the enbodiments.And it is extended from this it is obvious variation or
It changes still within the protection scope of the invention.
Claims (1)
1. a kind of turn emitter, which is characterized in that including
Emitter ontology (1) is equipped with first order kinetics medium (2) in inner cavity；
Emitting head (3), setting is in the front end of the emitter ontology (1), the emitting head (3) and the emitter ontology (1)
Between be equipped with thermal insulation layer (4), second motive force medium (5) are equipped in the inner cavity of the emitting head (3) and for receiving excitation control
Instruct the excitation structure to excite the second motive force medium (5)；
Emitting head (3) circumferential direction is equipped at least one injection channel (6), and one end of the injection channel (6) is connected to
The second motive force medium (5), the other end are penetrated through to the injection channel (6) of the emitting head (3) lateral outer；
The excitation structure includes: the double gold plaques (8) being mounted in the emitting head (3) inner cavity, thermally conductive excitation bar (9) and accommodating
There is the power house (10) of the second motive force medium (5)；The thermally conductive excitation bar (9) and double gold plaques (8) are arranged described
On power house (10), and the power house (10) is equipped with the spelling being detachably connected with the bullet shell (7) of the emitting head (3)
Assembling structure；
Described thermally conductive excitation bar (9) one end connects the second motive force medium (5), and the other end is opposite with double gold plaques (8) to be set
It sets, gap is equipped between double gold plaques (8) and the thermally conductive excitation bar (9), double gold plaque (8) temperature distortions are and described
Thermally conductive excitation bar (9) is connected；
The bottom of the emitting head (3) is equipped with the installing port (11) for installing the excitation structure；
The power house (10) is arranged at the installing port (11), and the transmitting of sealing structure is surrounded with the bullet shell (7)
Head (3)；
The splicing structure includes being separately positioned on the edge and the power house (10) of the installing port (11), phase interworking
Close connected helicitic texture；
The emitting head (3) is made of metal material；The power house (10) is made of heat insulator；
The thermally conductive excitation bar (9) protrudes into the power house (10) outside the power house (10) and is situated between with the second motive force
Matter (5) connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810647632.5A CN108931164A (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810647632.5A CN108931164A (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
| CN201710570954.XA CN107144178B (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710570954.XA Division CN107144178B (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108931164A true CN108931164A (en) | 2018-12-04 |
Family
ID=59776192
Family Applications (21)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810647563.8A Withdrawn CN108731552A (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
| CN201810647705.0A Withdrawn CN108759585A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
| CN201810647704.6A Withdrawn CN108871106A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
| CN201810647633.XA Withdrawn CN108731553A (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
| CN201810647701.2A Withdrawn CN108955419A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
| CN201810647762.9A Withdrawn CN108759586A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
| CN201810647632.5A Withdrawn CN108931164A (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
| CN201810647270.XA Withdrawn CN108871104A (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
| CN201810647763.3A Withdrawn CN108955424A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
| CN201810647564.2A Withdrawn CN108801077A (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
| CN201810647634.4A Withdrawn CN108931162A (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
| CN201710570954.XA Active CN107144178B (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
| CN201810647635.9A Withdrawn CN108871105A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
| CN201810647561.9A Withdrawn CN108801076A (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
| CN201810647764.8A Withdrawn CN108955420A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
| CN201810647562.3A Withdrawn CN108931160A (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
| CN201810647565.7A Withdrawn CN108955418A (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
| CN201810647703.1A Withdrawn CN108759584A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
| CN201810647761.4A Withdrawn CN108871107A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
| CN201810647702.7A Withdrawn CN108931163A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
| CN201810647631.0A Withdrawn CN108931161A (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810647563.8A Withdrawn CN108731552A (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
| CN201810647705.0A Withdrawn CN108759585A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
| CN201810647704.6A Withdrawn CN108871106A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
| CN201810647633.XA Withdrawn CN108731553A (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
| CN201810647701.2A Withdrawn CN108955419A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
| CN201810647762.9A Withdrawn CN108759586A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201810647270.XA Withdrawn CN108871104A (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
| CN201810647763.3A Withdrawn CN108955424A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
| CN201810647564.2A Withdrawn CN108801077A (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
| CN201810647634.4A Withdrawn CN108931162A (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
| CN201710570954.XA Active CN107144178B (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
| CN201810647635.9A Withdrawn CN108871105A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
| CN201810647561.9A Withdrawn CN108801076A (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
| CN201810647764.8A Withdrawn CN108955420A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
| CN201810647562.3A Withdrawn CN108931160A (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
| CN201810647565.7A Withdrawn CN108955418A (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
| CN201810647703.1A Withdrawn CN108759584A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
| CN201810647761.4A Withdrawn CN108871107A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
| CN201810647702.7A Withdrawn CN108931163A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
| CN201810647631.0A Withdrawn CN108931161A (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
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| CN (21) | CN108731552A (en) |
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| CN112179215B (en) * | 2020-09-21 | 2023-03-21 | 西安理工大学 | Flight guidance weapon control device based on plasma jet technology |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6871594B1 (en) * | 2003-04-01 | 2005-03-29 | Randall P. Estrella | Reusable paint grenade |
| DE102005043078B4 (en) * | 2005-09-10 | 2007-06-14 | Diehl Bgt Defence Gmbh & Co. Kg | Sensor fused munition |
| WO2014146170A1 (en) * | 2013-03-19 | 2014-09-25 | Van Reesema Fergus William Siewertsz | Projectile with rotational motion |
| CN105318794B (en) * | 2014-07-31 | 2017-04-19 | 南京理工大学 | Deflection warhead |
| CN205537363U (en) * | 2016-01-25 | 2016-08-31 | 杨杰 | Bullet |
| CN105674812B (en) * | 2016-01-29 | 2017-07-14 | 王海龙 | A kind of emitter and emitter |
-
2017
- 2017-07-13 CN CN201810647563.8A patent/CN108731552A/en not_active Withdrawn
- 2017-07-13 CN CN201810647705.0A patent/CN108759585A/en not_active Withdrawn
- 2017-07-13 CN CN201810647704.6A patent/CN108871106A/en not_active Withdrawn
- 2017-07-13 CN CN201810647633.XA patent/CN108731553A/en not_active Withdrawn
- 2017-07-13 CN CN201810647701.2A patent/CN108955419A/en not_active Withdrawn
- 2017-07-13 CN CN201810647762.9A patent/CN108759586A/en not_active Withdrawn
- 2017-07-13 CN CN201810647632.5A patent/CN108931164A/en not_active Withdrawn
- 2017-07-13 CN CN201810647270.XA patent/CN108871104A/en not_active Withdrawn
- 2017-07-13 CN CN201810647763.3A patent/CN108955424A/en not_active Withdrawn
- 2017-07-13 CN CN201810647564.2A patent/CN108801077A/en not_active Withdrawn
- 2017-07-13 CN CN201810647634.4A patent/CN108931162A/en not_active Withdrawn
- 2017-07-13 CN CN201710570954.XA patent/CN107144178B/en active Active
- 2017-07-13 CN CN201810647635.9A patent/CN108871105A/en not_active Withdrawn
- 2017-07-13 CN CN201810647561.9A patent/CN108801076A/en not_active Withdrawn
- 2017-07-13 CN CN201810647764.8A patent/CN108955420A/en not_active Withdrawn
- 2017-07-13 CN CN201810647562.3A patent/CN108931160A/en not_active Withdrawn
- 2017-07-13 CN CN201810647565.7A patent/CN108955418A/en not_active Withdrawn
- 2017-07-13 CN CN201810647703.1A patent/CN108759584A/en not_active Withdrawn
- 2017-07-13 CN CN201810647761.4A patent/CN108871107A/en not_active Withdrawn
- 2017-07-13 CN CN201810647702.7A patent/CN108931163A/en not_active Withdrawn
- 2017-07-13 CN CN201810647631.0A patent/CN108931161A/en not_active Withdrawn
Also Published As
| Publication number | Publication date |
|---|---|
| CN108955420A (en) | 2018-12-07 |
| CN107144178A (en) | 2017-09-08 |
| CN108871107A (en) | 2018-11-23 |
| CN108955418A (en) | 2018-12-07 |
| CN108731552A (en) | 2018-11-02 |
| CN108731553A (en) | 2018-11-02 |
| CN108801076A (en) | 2018-11-13 |
| CN108955419A (en) | 2018-12-07 |
| CN108871105A (en) | 2018-11-23 |
| CN107144178B (en) | 2018-10-02 |
| CN108871106A (en) | 2018-11-23 |
| CN108759585A (en) | 2018-11-06 |
| CN108931162A (en) | 2018-12-04 |
| CN108801077A (en) | 2018-11-13 |
| CN108759586A (en) | 2018-11-06 |
| CN108931163A (en) | 2018-12-04 |
| CN108871104A (en) | 2018-11-23 |
| CN108931160A (en) | 2018-12-04 |
| CN108759584A (en) | 2018-11-06 |
| CN108931161A (en) | 2018-12-04 |
| CN108955424A (en) | 2018-12-07 |
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Application publication date: 20181204 |