CN108731552A - A kind of turn emitter - Google Patents
A kind of turn emitter Download PDFInfo
- Publication number
- CN108731552A CN108731552A CN201810647563.8A CN201810647563A CN108731552A CN 108731552 A CN108731552 A CN 108731552A CN 201810647563 A CN201810647563 A CN 201810647563A CN 108731552 A CN108731552 A CN 108731552A
- Authority
- CN
- China
- Prior art keywords
- emitting head
- heat conduction
- bar
- excitation
- emitter
- 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.)
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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, including：Emitter ontology is equipped with first order kinetics medium in inner cavity；Emitting head, it is arranged in the front end of the emitter ontology, 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, are suitable for the emitter of non-rotating advance, and in particular to a kind of turn
Emitter.
Background technology
Emitter in the prior art includes mainly 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 there are shelter in front of object, emitter is launched from bore
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 disclose 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 block 105, the front end of the bullet seat 104 be provided with installation cavity, the bullet block 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 is extend into across the cavity 105 in the channel 103, and cannot be to hair by the limitation of the channel 103
It moves the rear end of beam；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, to be run forwards by the front-end driven bullet cut-through object of drive rod, 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 relatively low, 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.
Invention content
Therefore, the technical problem to be solved in the present invention is that overcoming emitter in the prior art to be easily blocked object blocks
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, are arranged in the front end of the emitter ontology,
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：Double gold plaques, heat conduction in the emitting head inner cavity excite bar and house
State the power house of second motive force medium；The heat conduction 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；
Heat conduction 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 heat conduction excitation bar, double gold plaque temperature distortions are connected with heat conduction 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 heat conduction excitation bar stretches into the power house outside the power house and is connect with the second motive force medium.
The power house upper end is equipped with the storage tank that bar is excited for being embedded in the heat conduction, the storage tank and double gold
Piece surrounds the accommodation chamber of the accommodating heat conduction excitation bar.
The storage tank is equipped with the extension channel extended towards the injection channel, and the lower end for extending channel is equipped with
Opening, the heat conduction excitation bar pass through the opening to be connected with the second motive force medium.
The second motive force medium is propellant powder, and sealing wax is filled in the injection channel.
The emitter is bullet.
Technical scheme of the present invention has the following 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
Excite control instruction 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：Double gold plaques in emitting head inner cavity,
Heat conduction excites bar and the power house for being equipped with second motive force medium；Heat conduction excites bar one end to connect second motive force medium, the other end
It is oppositely arranged with double gold plaques, gap is equipped between double gold plaques and heat conduction excitation bar, double gold plaque temperature distortions excite bar phase with heat conduction
Even.When emitting head in-flight, double gold plaques excite bar because air drag temperature is overcome to gradually rise generation temperature distortion, with heat conduction
It is connected, heat conduction 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 heat conduction excitation bar can just ignite in bullet after emitting head flight a period of time, user can replace double as needed
Gold plaque, heat conduction 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, installing port is arranged in the bottom of emitting head, and the bottom of bullet shell
It is made of power house, installs the power house of double gold plaques and heat conduction excitation bar, can quickly and easily be 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 storage tank that bar is excited for being embedded in heat conduction, holds
It sets slot and double gold plaques surrounds the accommodation chamber of accommodating heat conduction 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 heat conduction excitation bar only when double gold plaques continue temperature distortion
Heat conduction excitation bar is passed to, the opening that heat conduction excitation bar is then passed through accommodating trench bottom lights second motive force medium.Accommodation chamber can be with
Play the role of completely cutting off heat conduction excitation bar, heat conduction excitation bar is avoided voluntarily to excite second motive force medium.
5. turn emitter provided by the invention, the slot bottom of storage tank is additionally provided with the extension extended towards injection channel and leads to
Road extends channel lower end and is equipped with opening, and heat conduction excitation bar passes through opening to be 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 is pushed away to bullet turn
Action is used.
Description of the drawings
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 are briefly described, it should be apparent that, in being 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, other drawings may also be obtained 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 that heat conduction provided by the invention excites bar；
Fig. 6 is the structural schematic diagram of turn bullet in the prior art.
Reference sign：
1- emitter ontologies；2- first order kinetics media；3- emitting heads；4- thermal insulation layers；5- second motive force media；6- injections are logical
Road；7- bullet shells；The bis- gold plaques of 8-；9- heat conduction excites bar；10- power houses；11- installing ports；12- storage tanks；13- extends logical
Road；14- is open；101- bodies；102- warhead-containing bodies；The channels 103-；104- bullet seats；105- bullet blocks；106- movable blocks；
107- driving devices；108- drive seats；109- drive rods
Specific implementation mode
Technical scheme 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
The every other embodiment that personnel are 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；
Emitting head 3 made of metal is arranged in the front end of emitter ontology 1, emitting head 3 and emitter ontology 1
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；
It is set in 3 circumferential direction of emitting head there are one injection channel 6, injection channel 6 is interior to be filled with sealing wax, 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：Double gold plaques 8, heat conduction in 3 inner cavity of emitting head
Excitation bar 9 and the power house 10 for being equipped with propellant powder；Heat conduction excites bar 9 and double gold plaques 8 to be 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.Installing port is arranged in the bottom of emitting head,
And the bottom of bullet shell is made of power house, installs the power house of double gold plaques and heat conduction excitation bar, 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.
Heat conduction excites 9 one end of bar to connect propellant powder, and the other end is oppositely arranged with double gold plaques 8, and double gold plaques 8 and heat conduction excite bar
Gap is equipped between 9,8 temperature distortion of double gold plaques is connected with heat conduction 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 heat conduction excitation bar, and heat conduction excitation bar transfers heat to transmitting
Medicine pushes emitting head to turn round to light propellant powder.Heat conduction excitation bar can just ignite bullet after emitting head flight a period of time
Interior dynamic medium, user can replace as needed double gold plaques, heat conduction 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 of bar 9 is excited for being embedded in heat conduction
Slot 12, storage tank 12 and double gold plaques 8 surround the accommodation chamber of accommodating heat conduction 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 heat conduction excitation bar
Afterwards, heat conduction excitation bar can be just transferred heat to, the opening that heat conduction excitation bar is then passed through accommodating trench bottom lights propellant powder.It is accommodating
Room can play the role of completely cutting off heat conduction excitation bar, avoid heat conduction excitation bar voluntarily excitation-emission medicine.
Storage tank 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, heat conduction excitation bar 9 passes through opening 14 to be connected with propellant powder.To make heat conduction excitation bar 9 stretch into power outside power house 10
It is connect with propellant powder behind room 10.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；
Emitting head 3 made of metal is arranged in the front end of emitter ontology 1, emitting head 3 and emitter ontology 1
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；
It is set in 3 circumferential direction of emitting head there are one injection channel 6, injection channel 6 is interior to be filled with sealing wax, 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：Double gold plaques 8, heat conduction in 3 inner cavity of emitting head excite bar 9
With the power house 10 for being equipped with propellant powder；Heat conduction excites bar 9 and double gold plaques 8 to be 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 surrounds the emitting head 3 of sealing structure with bullet shell 7.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 heat conduction excitation bar, can quickly and easily 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.
Heat conduction excites 9 one end of bar to connect propellant powder, and the other end is oppositely arranged with double gold plaques 8, and double gold plaques 8 and heat conduction excite bar
Gap is equipped between 9,8 temperature distortion of double gold plaques is connected with heat conduction 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 heat conduction excitation bar, and heat conduction excitation bar transfers heat to transmitting
Medicine pushes emitting head to turn round to light propellant powder.Heat conduction excitation bar can just ignite bullet after emitting head flight a period of time
Interior dynamic medium, user can replace as needed double gold plaques, heat conduction 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) is equipped in the inner cavity of the emitting head (3) and for receiving excitation control
Instruction is to excite the excitation structure of 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：Double gold plaques (8), heat conduction in the emitting head (3) inner cavity excite bar (9) and house
There is the power house (10) of the second motive force medium (5)；The heat conduction 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；
Heat conduction 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, is equipped with gap between double gold plaques (8) and heat conduction excitation bar (9), double gold plaque (8) temperature distortions are and described
Heat conduction excites bar (9) to be connected；
The second motive force medium (5) is propellant powder, and sealing wax is filled in the injection channel (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810647563.8A CN108731552A (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710570954.XA CN107144178B (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
| CN201810647563.8A CN108731552A (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 |
|---|---|
| CN108731552A true CN108731552A (en) | 2018-11-02 |
Family
ID=59776192
Family Applications (21)
| Application Number | Title | Priority Date | Filing Date |
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| CN201810647705.0A Withdrawn CN108759585A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
| CN201810647701.2A Withdrawn CN108955419A (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 |
| CN201810647631.0A Withdrawn CN108931161A (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
| CN201810647563.8A Withdrawn CN108731552A (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 |
| CN201810647763.3A Withdrawn CN108955424A (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 |
| CN201810647761.4A Withdrawn CN108871107A (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 |
| CN201810647562.3A Withdrawn CN108931160A (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 |
| CN201810647634.4A Withdrawn CN108931162A (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
| CN201810647633.XA Withdrawn CN108731553A (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
| CN201810647702.7A Withdrawn CN108931163A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
| CN201810647762.9A Withdrawn CN108759586A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
| CN201810647703.1A Withdrawn CN108759584A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
| CN201810647764.8A Withdrawn CN108955420A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
| CN201810647270.XA Withdrawn CN108871104A (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
| CN201810647704.6A Withdrawn CN108871106A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
Family Applications Before (4)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810647705.0A Withdrawn CN108759585A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
| CN201810647701.2A Withdrawn CN108955419A (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 |
| CN201810647631.0A Withdrawn CN108931161A (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
Family Applications After (16)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810647565.7A Withdrawn CN108955418A (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 |
| CN201810647561.9A Withdrawn CN108801076A (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
| CN201810647761.4A Withdrawn CN108871107A (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 |
| CN201810647562.3A Withdrawn CN108931160A (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 |
| CN201810647634.4A Withdrawn CN108931162A (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
| CN201810647633.XA Withdrawn CN108731553A (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
| CN201810647702.7A Withdrawn CN108931163A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
| CN201810647762.9A Withdrawn CN108759586A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
| CN201810647703.1A Withdrawn CN108759584A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
| CN201810647764.8A Withdrawn CN108955420A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
| CN201810647270.XA Withdrawn CN108871104A (en) | 2017-07-13 | 2017-07-13 | A kind of turn emitter |
| CN201810647704.6A Withdrawn CN108871106A (en) | 2017-07-13 | 2017-07-13 | Turn emitter |
Country Status (1)
| Country | Link |
|---|---|
| CN (21) | CN108759585A (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
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2017
- 2017-07-13 CN CN201810647705.0A patent/CN108759585A/en not_active Withdrawn
- 2017-07-13 CN CN201810647701.2A patent/CN108955419A/en not_active Withdrawn
- 2017-07-13 CN CN201810647564.2A patent/CN108801077A/en not_active Withdrawn
- 2017-07-13 CN CN201810647631.0A patent/CN108931161A/en not_active Withdrawn
- 2017-07-13 CN CN201810647563.8A patent/CN108731552A/en not_active Withdrawn
- 2017-07-13 CN CN201810647565.7A patent/CN108955418A/en not_active Withdrawn
- 2017-07-13 CN CN201810647763.3A patent/CN108955424A/en not_active Withdrawn
- 2017-07-13 CN CN201810647561.9A patent/CN108801076A/en not_active Withdrawn
- 2017-07-13 CN CN201810647761.4A patent/CN108871107A/en not_active Withdrawn
- 2017-07-13 CN CN201810647632.5A patent/CN108931164A/en not_active Withdrawn
- 2017-07-13 CN CN201810647562.3A patent/CN108931160A/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 CN201810647634.4A patent/CN108931162A/en not_active Withdrawn
- 2017-07-13 CN CN201810647633.XA patent/CN108731553A/en not_active Withdrawn
- 2017-07-13 CN CN201810647702.7A patent/CN108931163A/en not_active Withdrawn
- 2017-07-13 CN CN201810647762.9A patent/CN108759586A/en not_active Withdrawn
- 2017-07-13 CN CN201810647703.1A patent/CN108759584A/en not_active Withdrawn
- 2017-07-13 CN CN201810647764.8A patent/CN108955420A/en not_active Withdrawn
- 2017-07-13 CN CN201810647270.XA patent/CN108871104A/en not_active Withdrawn
- 2017-07-13 CN CN201810647704.6A patent/CN108871106A/en not_active Withdrawn
Also Published As
| Publication number | Publication date |
|---|---|
| CN108931162A (en) | 2018-12-04 |
| CN108759586A (en) | 2018-11-06 |
| CN108931163A (en) | 2018-12-04 |
| CN108871106A (en) | 2018-11-23 |
| CN108731553A (en) | 2018-11-02 |
| CN108955424A (en) | 2018-12-07 |
| CN107144178A (en) | 2017-09-08 |
| CN108931160A (en) | 2018-12-04 |
| CN108871107A (en) | 2018-11-23 |
| CN107144178B (en) | 2018-10-02 |
| CN108759584A (en) | 2018-11-06 |
| CN108955420A (en) | 2018-12-07 |
| CN108931164A (en) | 2018-12-04 |
| CN108955419A (en) | 2018-12-07 |
| CN108871104A (en) | 2018-11-23 |
| CN108931161A (en) | 2018-12-04 |
| CN108801076A (en) | 2018-11-13 |
| CN108871105A (en) | 2018-11-23 |
| CN108801077A (en) | 2018-11-13 |
| CN108759585A (en) | 2018-11-06 |
| CN108955418A (en) | 2018-12-07 |
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