CN109596009A - The anti-riot howitzer of plural serial stage push type composite strike type - Google Patents
The anti-riot howitzer of plural serial stage push type composite strike type Download PDFInfo
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- CN109596009A CN109596009A CN201811654994.3A CN201811654994A CN109596009A CN 109596009 A CN109596009 A CN 109596009A CN 201811654994 A CN201811654994 A CN 201811654994A CN 109596009 A CN109596009 A CN 109596009A
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- Prior art keywords
- level
- pinking
- promotion part
- delay tube
- tear
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- 239000003491 tear gas Substances 0.000 claims abstract description 134
- 239000000779 smoke Substances 0.000 claims abstract description 45
- 238000010008 shearing Methods 0.000 claims abstract description 13
- 239000003380 propellant Substances 0.000 claims description 77
- 239000000843 powder Substances 0.000 claims description 48
- 239000000446 fuel Substances 0.000 claims description 20
- 229910000831 Steel Inorganic materials 0.000 claims description 16
- 239000010959 steel Substances 0.000 claims description 16
- 238000007789 sealing Methods 0.000 claims description 15
- 230000000638 stimulation Effects 0.000 claims description 14
- 239000003795 chemical substances by application Substances 0.000 claims description 13
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/46—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing gases, vapours, powders or chemically-reactive substances
- F42B12/48—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing gases, vapours, powders or chemically-reactive substances smoke-producing, e.g. infrared clouds
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/02—Stabilising arrangements
- F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/42—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information of illuminating type, e.g. carrying flares
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/46—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing gases, vapours, powders or chemically-reactive substances
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Toys (AREA)
Abstract
The invention discloses the anti-riot howitzers of plural serial stage push type composite strike type, it include: shell case, emission part, Delay Tube, promotion part, missile wing, shear screw thread, pinking portion, booster box, smoke portion, tear-gas portion and kinetic energy portion, the shell case and pinking portion are threadedly coupled by shearing, the emission part assigns flight initial velocity, the Delay Tube quantity is four, for lighting a fire in due course, the missile wing ensures flight stability, the promotion part quantity is two, propulsive acceleration is successively assigned twice, the pinking portion is for issuing the deterrence sound and intense flash, the booster is for casting pinking portion aside, the smoke portion is for generating interference smog, the tear-gas portion disperses for realizing tear-gas, the kinetic energy portion is for realizing kinetic energy strike, between two promotion parts of the invention, it is connected between four Delay Tubes using tandem, it is under fire in succession , realize fright, smoke, tear-gas, kinetic energy strike it is compound it is non-lethal disperse effect, 600 meters of range, be suitable for the prominent task in remote anti-riot place.
Description
Technical field
The present invention relates to anti-riot equipment technology fields, more specifically, more particularly to plural serial stage push type composite strike
The anti-riot howitzer of type.
Background technique
Howitzer belongs to tactical offensive type Suppressed Weapons, after transmitting, fuse reed time controll projectile explosion on bullet, to suppress,
Destroy the cluster effective strength of enemy, Tank and Armoured Vehicle, gun emplacement, airport installation, command communication system, radar site,
The targets such as underground fortification, surface ship group.By implementing medium-long range strike to the biggish target of these areas, keep it permanent
Or temporarily funeral makes fight function, achievees the purpose that eliminate enemy or delays enemy's operation.Anti-riot howitzer is equally beaten using face
The mode of hitting carries out sudden and violent riot crowd and disperses, it can also be used to expel the suspect concealed in closing or hemi-closure space.It is anti-riot
The antiriot bomb of the relatively traditional simple function of howitzer is sent out for tear bombnoun, kinetic energy weapon, smoke projectile, pinking bullet by dedicated howitzer
Emitter is emitted, and tactical qualities are more superior.
Anti-riot howitzer is as common anti-riot equipment, because its is of simple structure and low cost, be suitable for various emergency situations and
Anti-riot demand also has preferable application for the marine right-safeguarding task that carries out especially suitable for the disposition of extensive sudden and violent riot
Prospect, but existing anti-riot howitzer has a single function, range is shorter, tactics flexibility is poor, Shang Buneng successfully manages increasingly complicated
Place is prominent, anti-terrorism situation, in view of this, studied improvement for existing problem, provide that plural serial stage push type is compound to be beaten
Hit the anti-riot howitzer of type, it is intended to by the technology, achieve the purpose that solve realistic problem and improve tactical qualities.
Summary of the invention
The purpose of the present invention is to provide the anti-riot howitzers of plural serial stage push type composite strike type, to solve above-mentioned background skill
The existing anti-riot howitzer proposed in art has a single function, range is shorter, the problem of tactics flexibility difference.
To achieve the above object, the present invention provides the anti-riot howitzers of plural serial stage push type composite strike type, by following tool
Body technique means are reached:
The anti-riot howitzer of plural serial stage push type composite strike type, comprising: shell case, emission part, screw-in screw thread, mechanical impact
The formula fire in a stove before fuel is added, hyperbaric chamber, propellant powder, sealing cover foil, flash hole, low-pressure chamber, level-one Delay Tube, level-one promotion part, level-one promotion part
Propellant chamber, level-one promotion part propellant, level-one promotion part nozzle, level-one promotion part lower end Delay Tube jack, level-one promote
Portion upper end Delay Tube jack, missile wing, missile wing shaft, torsionspring, second level Delay Tube, shears screw thread, is quick-fried level-one promotion part outer wall
Shake portion, pinking portion steel body, pinking portion papery shell case, pinking chamber, pinking chamber lid, blast hole, glitter, the expansion of pinking portion are quick-fried
Pipe, pinking portion propagation squib relief hole, pinking portion booster, pinking portion bonding place, pinking subordinate end Delay Tube jack, in pinking portion
Delay Tube jack, three-level Delay Tube, booster box, second level promotion part, second level promotion part propellant chamber, second level promotion part is held to promote
It is agent, second level promotion part upper end Delay Tube jack, second level promotion part nozzle, fire jetting hole, smoke portion, smoke-pot, smoke agent, oblique
Fumarole, level Four Delay Tube, tear-gas portion, tear-gas portion propagation squib, tear-gas portion propagation squib radial direction relief hole, tear-gas portion propagation squib are axial
Relief hole, tear-gas portion stimulation powder chamber, OC stimulation powder, tear-gas subordinate end Delay Tube jack, kinetic energy portion, moves tear-gas portion booster
Energy portion shell, rubber bullet and arch blast cap；It is characterized by: the shell case and pinking portion are threadedly coupled by shearing, it is described
Emission part is set on the central axes of shell case lower end, and the emission part includes screw-in screw thread, the mechanical impact formula fire in a stove before fuel is added, high pressure
Room, propellant powder and sealing cover foil, the emission part and shell case are threadedly coupled by screw-in and are fixed, the mechanical impact formula fire in a stove before fuel is added
It is riveted on the central axes of emission part bottom end, is provided with hyperbaric chamber on the upside of the mechanical impact formula fire in a stove before fuel is added, the hyperbaric chamber is built-in
Propellant powder, the hyperbaric chamber are sealed by sealing cover foil, are intensively provided in the sealing cover foil small by the pressure release of hot melt adhesive sealing
The lower end surface of hole, the emission part and shell case is evened up, and the low-pressure chamber is connected to by flash hole with hyperbaric chamber, the shell case top
Level-one promotion part is provided on the upside of inside, low-pressure chamber, the level-one promotion part insertion is mounted on pinking subordinate portion, and the level-one pushes away
It include that level-one promotion part propellant chamber, level-one promotion part propellant, level-one promotion part nozzle, level-one promotion part lower end are prolonged into portion
Phase pipe jack, level-one promotion part upper end Delay Tube jack and level-one promotion part outer wall, level-one promotion part propellant chamber are built-in
Level-one promotion part propellant, the level-one promotion part propellant chamber lower end surface are provided with level-one promotion part nozzle, the level-one
Promotion part lower end Delay Tube jack is inserted with level-one Delay Tube, and level-one promotion part upper end Delay Tube jack is inserted with second level extension
Pipe, level-one Delay Tube front are located inside low-pressure chamber, and level-one Delay Tube rear portion is located at level-one promotion part propellant chamber
Inside, the shell case upper inner, level-one promotion part outer exterior wall are provided with missile wing, and the missile wing includes missile wing shaft and torsion
Spring, the level-one promotion part upside are provided with pinking portion, and the pinking portion includes pinking portion steel body, pinking portion papery bullet
Shell, pinking chamber, pinking chamber lid, blast hole, glitter, pinking portion propagation squib, pinking portion booster, pinking portion bonding place, pinking
Subordinate end Delay Tube jack and pinking portion upper end Delay Tube jack, the pinking portion steel body depression in centre section outside are enclosed with
Pinking portion papery shell case, the pinking portion papery shell case outer are evened up with pinking portion steel body outer, pinking portion axis
Pinking portion propagation squib, the built-in pinking portion booster of pinking portion propagation squib, the pinking portion propagation squib tube wall are provided on line
On be provided with pinking portion propagation squib relief hole, be provided with pinking chamber on the outside of pinking portion propagation squib, the pinking chamber is by pinking
Chamber lid sealing, the intracavitary dress glitter of pinking, the pinking cavity outer wall are provided with blast hole, and the pinking portion is viscous in pinking portion
It is fixed at conjunction with smoke portion gluing, pinking subordinate end Delay Tube jack is inserted with the second stage of Delay Tube, and the pinking portion prolongs upper end
Phase pipe jack is inserted with three-level Delay Tube, and the second phase Delay Tube front is located inside the propellant chamber of level-one promotion part, the second phase
Delay Tube rear portion is located at pinking portion after being sequentially inserted into level-one promotion part upper end Delay Tube jack and pinking subordinate end Delay Tube jack
Inside propagation squib, three-level Delay Tube front is located inside pinking portion propagation squib, and it is quick-fried that three-level Delay Tube rear portion is located at expansion
Inside medicine box, be provided with second level promotion part on the upside of the pinking portion, the second level promotion part include second level promotion part propellant chamber,
Second level promotion part propellant, second level promotion part upper end Delay Tube jack, second level promotion part nozzle and fire jetting hole, the second level push away
Into the built-in second level promotion part propellant of portion's propellant chamber, second level promotion part upper end Delay Tube jack is inserted with level Four Delay Tube,
Second level promotion part lower end surface is provided with second level promotion part nozzle, and the fire jetting hole is by second level promotion part propellant chamber and hair
The cavity that the connection of cigarette portion, pinking portion upper surface and second level promotion part lower end surface are constituted is booster box, the booster
Box built-in booster on the upside of the pinking portion, is provided with smoke portion on the outside of second level promotion part, the smoke portion include smoke-pot,
Smoke agent and oblique fumarole, the smoke-pot are open circles cyclic structure, and the smoke-pot inside is against second level promotion part, institute
The built-in smoke agent of smoke-pot is stated, oblique fumarole is provided on the outside of the smoke-pot, is provided with and urges on the upside of the second level promotion part
Tear portion, the tear-gas portion include tear-gas portion propagation squib, tear-gas portion booster, tear-gas portion stimulation powder chamber, OC stimulation powder and tear-gas
Subordinate end Delay Tube jack, tear-gas portion propagation squib are located on tear-gas portion central axes, set on the tear-gas portion propagation squib tube wall
It is equipped with tear-gas portion propagation squib radial direction relief hole and tear-gas portion propagation squib axial direction relief hole, the built-in tear-gas portion of tear-gas portion propagation squib
Booster, tear-gas portion outer wall, which constitutes tear-gas portion, stimulates powder chamber, and the intracavitary dress OC of the tear-gas portion stimulation powder stimulates powder, described
Tear-gas subordinate end Delay Tube jack is inserted with level Four Delay Tube, and the front of the level Four Delay Tube is located at second level promotion part propellant chamber
Inside, level Four Delay Tube rear portion are sequentially inserted into second level promotion part upper end Delay Tube jack and tear-gas subordinate end Delay Tube jack
It is located inside tear-gas portion propagation squib afterwards, is provided with kinetic energy portion on the outside of the tear-gas portion, the kinetic energy portion includes kinetic energy portion shell, rubber
Glue bullet and arch blast cap, the rubber bullet are cannonball, and the rubber bullet stimulates powder chamber and kinetic energy portion in tear-gas portion
Close-packed arrays in the space that shell is constituted, arch blast cap outer surface are convex spherical shape structure, are conducive to reduce windage.
As advanced optimizing for the technical program, the anti-riot howitzer of plural serial stage push type composite strike type of the present invention, institute
State shell case, screw-in screw thread, the mechanical impact formula fire in a stove before fuel is added, hyperbaric chamber, low-pressure chamber, level-one Delay Tube, level-one promotion part propellant chamber,
Level-one promotion part lower end Delay Tube jack, level-one promotion part upper end Delay Tube jack, second level Delay Tube shear screw thread, pinking portion steel
Matter body, pinking portion papery shell case, pinking chamber, pinking chamber lid, pinking portion propagation squib, pinking subordinate end Delay Tube jack, pinking
Portion upper end Delay Tube jack, three-level Delay Tube, booster box, second level promotion part propellant chamber, second level promotion part upper end Delay Tube
Jack, smoke-pot, level Four Delay Tube, tear-gas portion propagation squib, tear-gas portion stimulate powder chamber, tear-gas subordinate end Delay Tube jack, kinetic energy
The central axes of portion's shell and arch blast cap are overlapped, and level-one promotion part upper end Delay Tube jack and pinking subordinate end Delay Tube are inserted
Hole internal diameter is equal, up and down against, be mutually communicated, second level promotion part upper end Delay Tube jack and tear-gas subordinate end Delay Tube are inserted
Hole internal diameter is equal, up and down against, be mutually communicated.
As advanced optimizing for the technical program, the anti-riot howitzer of plural serial stage push type composite strike type of the present invention, institute
The quantity for stating flash hole, level-one promotion part nozzle, missile wing, second level promotion part nozzle and fire jetting hole is 4, and described 4
A flash hole, 4 level-one promotion part nozzles, 4 missile wings, 4 second level promotion part nozzles and 4 fire jetting holes are respectively along shell case
Central axes circumferentially formula array distribution.
As advanced optimizing for the technical program, the anti-riot howitzer of plural serial stage push type composite strike type of the present invention, institute
By the opposite against the missile wing compression torsionspring and quilt of shell case inner wall and level-one promotion part outer wall when stating missile wing original state
It buries and fills out inside shell case, turned along missile wing by torsionspring effect in shell case and pinking part from rear when the missile wing emission state
Axis rotates counterclockwise, abuts against the shearing screw thread in pinking subordinate portion, continues to act on because of torsionspring tension, in pinking portion
Axis constitutes 30 ° of constant subtended angles.
As advanced optimizing for the technical program, the anti-riot howitzer of plural serial stage push type composite strike type of the present invention, institute
It states blast hole and is provided with 5 on the same axial direction in pinking portion, 5 blast holes composition one in the same axial direction is quick-fried
Holes group, the quantity of the blast hole group are 8, and along the central axes in pinking portion, circumferentially formula array divides 8 blast hole groups
Cloth.
As advanced optimizing for the technical program, the anti-riot howitzer of plural serial stage push type composite strike type of the present invention, institute
It states oblique fumarole and is provided with 2 on the same axial direction in smoke portion, 2 oblique fumarole structures in the same axial direction
At an oblique fumarole group, the quantity of the oblique fumarole group is 8, and 8 oblique fumarole groups are along smoke portion
Central axes circumferentially formula array distribution.
As advanced optimizing for the technical program, the anti-riot howitzer of plural serial stage push type composite strike type of the present invention, institute
Stating pinking portion propagation squib relief hole is the aperture to gather on pinking portion propagation squib side wall, the tear-gas portion propagation squib radial direction pressure release
Hole is the aperture to gather on tear-gas portion propagation squib side wall, and the tear-gas portion propagation squib axial direction relief hole is to gather to expand in tear-gas portion
Aperture on booster roof.
As advanced optimizing for the technical program, the anti-riot howitzer of plural serial stage push type composite strike type of the present invention, institute
State a phase Delay Tube, second level Delay Tube, three-level Delay Tube and level Four Delay Tube the extension time be respectively as follows: 1.5S, 3S, 2S and
2S, the phase Delay Tube, second level Delay Tube, three-level Delay Tube and level Four Delay Tube are inserted by high-temperature plastic in each Delay Tube
It is securely held at hole.
As advanced optimizing for the technical program, the anti-riot howitzer of plural serial stage push type composite strike type of the present invention, institute
State flash hole, level-one promotion part nozzle, blast hole, pinking portion propagation squib relief hole, second level Delay Tube nozzle, fire jetting hole,
Oblique fumarole, tear-gas portion propagation squib radial direction relief hole and tear-gas portion propagation squib axial direction relief hole are sealed by hot melt adhesive.
As advanced optimizing for the technical program, the anti-riot howitzer of plural serial stage push type composite strike type of the present invention, institute
Shell case is stated by aluminum alloy materials processing and fabricating, the tear-gas portion stimulation powder chamber cavity wall and kinetic energy portion shell are processed by PVC material and made
Make.
Due to the application of the above technical scheme, compared with the prior art, the invention has the following advantages:
1. structure of the invention is ingenious, science novel in design；
2. the mechanical impact formula fire in a stove before fuel is added, hyperbaric chamber, propellant powder are integrated into an integral module by emission part of the invention, with bullet
Thread connecting mode is used between shell, shell case can be recycled, emission part be loaded again, Ji Kezai after each transmitting
Secondary use；
3. between two promotion parts of the invention, series connection mode is used between four Delay Tubes, by cleverly designing,
It realizes and is under fire in succession, realize and successively increase journey purpose twice；It is needed according to tactics simultaneously, it can be achieved that different in different flying distances
Effect is dispersed in the strike of non-lethal effect；
4. what the present invention designed, which buries, fills out formula torsional spring missile wing, the monnolithic case of body is not destroyed, by compressing torsionspring, is borrowed
Level-one promotion part outer wall and shell case upper inside wall is helped to collapse missile wing, the shearing screw thread between pinking portion and shell case is sheared
After destruction, missile wing rotates counterclockwise under the action of torsion spring force, is limited by pinking portion shearing screw thread, is in 30 ° of subtended angles,
Flight stability of the invention can be significantly increased；
5. the present invention is by design pinking portion, smoke portion, tear-gas portion and kinetic energy portion, can under different shooting distances,
Successively realize that fright, smog interference, tear-gas disperse and the multiple non-lethal effects such as kinetic energy strike, vdiverse in function, tactical qualities spirit
It is living.The present invention in 400 meters of flying distances, be under fire by pinking portion, issues the strong explosion sound and intense flash, subsequent pinking portion is expanded
It in quick-fried medicine box under the action of booster combustion gas, is pulled out away from, remaining body is continued to promote by second level promotion part, while smoke portion is sent out
Cigarette after flying to target area while realizing that tear-gas disperses and kinetic energy strike.
Detailed description of the invention
The attached drawing constituted part of this application is used to provide further understanding of the present invention, schematic reality of the invention
It applies example and its explanation is used to explain the present invention, do not constitute improper limitations of the present invention.In the accompanying drawings:
Fig. 1 is the structural diagram of the present invention；
Fig. 2 is the structural schematic diagram of emission part 2 in the present invention；
Fig. 3 is the structural schematic diagram of level-one promotion part 6 in the present invention；
Fig. 4 is the structural schematic diagram of missile wing 7 in the present invention；
Fig. 5 is the perspective view of torsionspring 7-2 in the present invention；
Fig. 6 is the structural schematic diagram in pinking portion 10 in the present invention；
Fig. 7 is the perspective view of pinking portion propagation squib 10-7 in the present invention；
Fig. 8 is the structural schematic diagram of second level promotion part 13 and smoke portion 14 in the present invention；
Fig. 9 is the structural schematic diagram in tear-gas portion 16 in the present invention；
Figure 10 is the perspective view of tear-gas portion propagation squib 16-1 in the present invention；
Figure 11 is the structural schematic diagram in kinetic energy portion 17 in the present invention.
In figure: 1, shell case, 2, emission part, 2-1, screw-in screw thread, 2-2, the mechanical impact formula fire in a stove before fuel is added, 2-3, hyperbaric chamber, 2-
4, propellant powder, 2-5, sealing cover foil, 3, flash hole, 4, low-pressure chamber, 5, level-one Delay Tube, 6, level-one promotion part, 6-1, level-one push away
Into portion's propellant chamber, 6-2, level-one promotion part propellant, 6-3, level-one promotion part nozzle, 6-4, level-one promotion part lower end are delayed
Pipe jack, 6-5, level-one promotion part upper end Delay Tube jack, 6-6, level-one promotion part outer wall, 7, missile wing, 7-1, missile wing shaft, 7-
2, torsionspring, 8, second level Delay Tube, 9, shearing screw thread, 10, pinking portion, 10-1, pinking portion steel body, 10-2, pinking portion
Papery shell case, 10-3, pinking chamber, 10-4, pinking chamber lid, 10-5, blast hole, 10-6, glitter, 10-7, pinking portion propagation squib,
10-7-1, pinking portion propagation squib relief hole, 10-8, pinking portion booster, 10-9, pinking portion bonding place, 10-10, pinking subordinate
Hold Delay Tube jack, 10-11, pinking portion upper end Delay Tube jack, 11, three-level Delay Tube, 12, booster box, 13, second level propulsion
Portion, 13-1, second level promotion part propellant chamber, 13-2, second level promotion part propellant, 13-3, second level promotion part upper end Delay Tube are inserted
Hole, 13-4, second level promotion part nozzle, 13-5, fire jetting hole, 14, smoke portion, 14-1, smoke-pot, 14-2, smoke agent, 14-3,
Oblique fumarole, 15, level Four Delay Tube, 16, tear-gas portion, 16-1, tear-gas portion propagation squib, 16-1-1, tear-gas portion propagation squib are radial
Relief hole, 16-1-2, tear-gas portion propagation squib axial direction relief hole, 16-2, tear-gas portion booster, 16-3, tear-gas portion stimulate powder chamber,
16-4, OC stimulate powder, 16-5, tear-gas subordinate end Delay Tube jack, 17, kinetic energy portion, 17-1, kinetic energy portion shell, 17-2, rubber
Bullet, 17-3, arch blast cap.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Fig. 1-11 is please referred to, the present invention provides a kind of technical solution: the anti-riot howitzer of plural serial stage push type composite strike type,
Including shell case 1, emission part 2, screw-in screw thread 2-1, mechanical impact formula fire in a stove before fuel is added 2-2, hyperbaric chamber 2-3, propellant powder 2-4, sealing cover
Foil 2-5, flash hole 3, low-pressure chamber 4, level-one Delay Tube 5, level-one promotion part 6, level-one promotion part propellant chamber 6-1, level-one promote
Portion propellant 6-2, level-one promotion part nozzle 6-3, level-one promotion part lower end Delay Tube jack 6-4, level-one promotion part upper end are prolonged
Phase pipe jack 6-5, level-one promotion part outer wall 6-6, missile wing 7, missile wing shaft 7-1, torsionspring 7-2, second level Delay Tube 8, shearing
Screw thread 9, pinking portion 10, pinking portion steel body 10-1, pinking portion papery shell case 10-2, pinking chamber 10-3, pinking chamber lid 10-4,
Blast hole 10-5, glitter 10-6, pinking portion propagation squib 10-7, pinking portion propagation squib relief hole 10-7-1, pinking portion booster
10-8, pinking portion bonding place 10-9, pinking subordinate end Delay Tube jack 10-10, pinking portion upper end Delay Tube jack 10-11, three
Grade Delay Tube 11, booster box 12, second level promotion part 13, second level promotion part propellant chamber 13-1, second level promotion part propellant 13-
2, second level promotion part upper end Delay Tube jack 13-3, second level promotion part nozzle 13-4, fire jetting hole 13-5, smoke portion 14, smoke
Tank 14-1, smoke agent 14-2, oblique fumarole 14-3, level Four Delay Tube 15, tear-gas portion 16, tear-gas portion propagation squib 16-1, tear-gas
Portion propagation squib radial direction relief hole 16-1-1, tear-gas portion propagation squib axial direction relief hole 16-1-2, tear-gas portion booster 16-2, tear-gas portion
Stimulate powder chamber 16-3, OC stimulate powder 16-4, tear-gas subordinate end Delay Tube jack 16-5, kinetic energy portion 17, kinetic energy portion shell 17-1,
Rubber bullet 17-2 and arch blast cap 17-3；It is characterized by: the shell case 1 is by aluminum alloy materials processing and fabricating, the shell case 1
It is connected with pinking portion 10 by shearing screw thread 9, setting shears the external screw thread of screw thread 9, is arranged in pinking portion 10 and cuts on shell case 1
The internal screw thread of chasing 9, the emission part 2 are set on 1 lower end central axes of shell case, and the emission part 2 includes screw-in spiral shell
Line 2-1, mechanical impact formula fire in a stove before fuel is added 2-2, hyperbaric chamber 2-3, propellant powder 2-4 and sealing cover foil 2-5, the emission part 2 and shell case 1 are logical
It crosses screw-in screw thread 2-1 to be connected and fixed, the mechanical impact formula fire in a stove before fuel is added 2-2 is riveted on 2 bottom end central axes of emission part, described
Hyperbaric chamber 2-3, the built-in propellant powder 2-4 of hyperbaric chamber 2-3, the hyperbaric chamber 2-3 are provided on the upside of mechanical impact formula fire in a stove before fuel is added 2-2
It is sealed by sealing cover foil 2-5, is densely covered with the relief hole sealed by hot melt adhesive, the emission part 2 and bullet on the sealing cover foil 2-5
The lower end surface of shell 1 is evened up, and the emission part 2 uses Modular Structure Design, after present invention percussion, can screw off emission part 2,
Mechanical impacting type fire in a stove before fuel is added 2-2 is loaded again, can be reused, reuse rate of the invention is improved, and the low-pressure chamber 4 is logical
It crosses flash hole 3 to be connected to hyperbaric chamber 2-3, is provided with level-one promotion part 6 on the upside of 1 upper inner of shell case, low-pressure chamber 4, it is described
The insertion of level-one promotion part 6 is mounted on 10 lower part of pinking portion, the level-one promotion part 6 and pinking portion 10 can also be processed into one it is whole
Body structure, the level-one promotion part 6 include level-one promotion part propellant chamber 6-1, level-one promotion part propellant 6-2, level-one propulsion
Portion nozzle 6-3, level-one promotion part lower end Delay Tube jack 6-4, level-one promotion part upper end Delay Tube jack 6-5 and level-one promote
Portion outer wall 6-6, the built-in level-one promotion part propellant 6-2 of level-one promotion part propellant chamber 6-1, the level-one promotion part promote
The lower end surface agent chamber 6-1 is provided with level-one promotion part nozzle 6-3, and level-one promotion part lower end Delay Tube jack 6-4 is inserted with one
Grade Delay Tube 5, level-one promotion part upper end Delay Tube jack 6-5 are inserted with second level Delay Tube 8,5 front of level-one Delay Tube
Inside low-pressure chamber 4,5 rear portion of level-one Delay Tube is located inside the propellant chamber 6-1 of level-one promotion part, on the shell case 1
Missile wing 7 is provided on the inside of portion, on the outside of the outer wall 6-6 of level-one promotion part, the missile wing 7 includes missile wing shaft 7-1 and torsionspring 7-
2, pinking portion 10 is provided on the upside of the level-one promotion part 6, the pinking portion 10 includes pinking portion steel body 10-1, pinking portion
Papery shell case 10-2, pinking chamber 10-3, pinking chamber lid 10-4, blast hole 10-5, glitter 10-6, pinking portion propagation squib 10-7,
Pinking portion booster 10-8, pinking portion bonding place 10-9, pinking subordinate end Delay Tube jack 10-10 and pinking portion upper end Delay Tube
Jack 10-11, the pinking portion steel body 10-1 depression in centre section outside is enclosed with pinking portion papery shell case 10-2, described quick-fried
The shake portion papery outer shell case 10-2 is evened up with the pinking portion outer steel body 10-1, is provided on 10 central axes of pinking portion quick-fried
Shake portion propagation squib 10-7, the built-in pinking portion booster 10-8 of pinking portion propagation squib 10-7, the pinking portion propagation squib 10-7
It is provided with pinking portion propagation squib relief hole 10-7-1 on tube wall, is provided with pinking chamber 10- on the outside of the pinking portion propagation squib 10-7
3, the pinking chamber 10-3 are sealed by pinking chamber lid 10-4, the built-in glitter 10-6 of pinking chamber 10-3, the pinking chamber 10-
3 outer walls are provided with blast hole 10-5, and the pinking portion 10 is fixed in pinking portion bonding place 10-9 and 14 gluing of smoke portion, described quick-fried
Shake subordinate end Delay Tube jack 10-10 is inserted with the second stage of Delay Tube 8, and pinking portion upper end Delay Tube jack 10-11 is inserted with three-level
Delay Tube 11,8 front of the second phase Delay Tube are located inside the propellant chamber 6-1 of level-one promotion part, 8 rear portion of the second phase Delay Tube
It is located at the expansion of pinking portion after being sequentially inserted into level-one promotion part upper end Delay Tube jack 6-5 and pinking subordinate end Delay Tube jack 10-10
Inside booster 10-7,11 front of three-level Delay Tube is located inside pinking portion propagation squib 10-7, after the three-level Delay Tube 11
Portion is located inside booster box 12, and second level promotion part 13 is provided on the upside of the pinking portion 10, and the second level promotion part 13 includes
Second level promotion part propellant chamber 13-1, second level promotion part propellant 13-2, second level promotion part upper end Delay Tube jack 13-3, second level
Promotion part nozzle 13-4 and fire jetting hole 13-5, the built-in second level promotion part propellant of second level promotion part propellant chamber 13-1
13-2, second level promotion part upper end Delay Tube jack 13-3 are inserted with level Four Delay Tube 15,13 lower end surface of second level promotion part
It is provided with second level promotion part nozzle 13-4, the fire jetting hole 13-5 connects second level promotion part propellant chamber 13-1 and smoke portion 14
Logical, the cavity that 10 upper surface of pinking portion and 13 lower end surface of second level promotion part are constituted is booster box 12, the booster
The built-in booster of box 12 is provided with smoke portion 14 on the outside of 10 upside of the pinking portion, second level promotion part 13, and the smoke portion 14 is wrapped
Smoke-pot 14-1, smoke agent 14-2 and oblique fumarole 14-3 are included, the smoke-pot 14-1 is open circles cyclic structure, the hair
On the inside of smoke cande 14-1 on the outside of second level promotion part 13, the built-in smoke agent 14-2 of smoke-pot 14-1, the smoke-pot 14-1
It is provided with oblique fumarole 14-3, tear-gas portion 16 is provided on the upside of the second level promotion part 13, the tear-gas portion 16 includes tear-gas
Portion propagation squib 16-1, tear-gas portion booster 16-2, tear-gas portion stimulation powder chamber 16-3, OC stimulate powder 16-4 and tear-gas subordinate end to prolong
Phase pipe jack 16-5, the tear-gas portion propagation squib 16-1 are located on 16 central axes of tear-gas portion, the tear-gas portion propagation squib 16-1 pipe
Tear-gas portion propagation squib radial direction relief hole 16-1-1 and tear-gas portion propagation squib axial direction relief hole 16-1-2, the tear-gas are provided on wall
The built-in tear-gas portion booster 16-2 of portion propagation squib 16-1,16 outer wall of tear-gas portion, which constitutes tear-gas portion, stimulates powder chamber 16-3, described
Tear-gas portion stimulates powder chamber 16-3 cavity wall by PVC material processing and fabricating, and the built-in OC of the tear-gas portion stimulation powder chamber 16-3 stimulates powder
16-4, tear-gas subordinate end Delay Tube jack 16-5 are inserted with level Four Delay Tube 15, and the front of the level Four Delay Tube 15 is located at
Inside the propellant chamber 13-1 of second level promotion part, 15 rear portion of level Four Delay Tube is sequentially inserted into second level promotion part upper end Delay Tube and inserts
It is located inside tear-gas portion propagation squib 16-1 after hole 13-3 and tear-gas subordinate end Delay Tube jack 16-5, is set on the outside of the tear-gas portion 16
It is equipped with kinetic energy portion 17, the kinetic energy portion 17 includes kinetic energy portion shell 17-1, rubber bullet 17-2 and arch blast cap 17-3, described dynamic
Energy portion shell 17-1 is cannonball by PVC material processing and fabricating, the rubber bullet 17-2, and the rubber bullet 17-2 is being urged
Close-packed arrays in the space that tear portion stimulates powder chamber 16-3 and kinetic energy portion shell 17-1 to constitute, the outer surface arch blast cap 17-3 is
Convex spherical shape structure is conducive to reduce windage.
Please refer to Fig. 1-11, the shell case 1, screw-in screw thread 2-1, mechanical impact formula fire in a stove before fuel is added 2-2, hyperbaric chamber 2-3, low pressure
Room 4, level-one Delay Tube 5, level-one promotion part propellant chamber 6-1, level-one promotion part lower end Delay Tube jack 6-4, level-one promotion part
Upper end Delay Tube jack 6-5, second level Delay Tube 8, shearing screw thread 9, pinking portion steel body 10-1, pinking portion papery shell case 10-
2, pinking chamber 10-3, pinking chamber lid 10-4, pinking portion propagation squib 10-7, pinking subordinate end Delay Tube jack 10-10, in pinking portion
Hold Delay Tube jack 10-11, three-level Delay Tube 11, booster box 12, second level promotion part propellant chamber 13-1, on second level promotion part
Hold Delay Tube jack 13-3, smoke-pot 14-1, level Four Delay Tube 15, tear-gas portion propagation squib 16-1, tear-gas portion stimulation powder chamber 16-3,
The central axes of tear-gas subordinate end Delay Tube jack 16-5, kinetic energy portion shell 17-1 and arch blast cap 17-3 are overlapped, and the level-one pushes away
It is equal into portion upper end Delay Tube jack 6-5 and pinking subordinate end Delay Tube jack 10-10 internal diameter, up and down against, be mutually communicated, institute
State second level promotion part upper end Delay Tube jack 13-3 and tear-gas subordinate end Delay Tube jack 16-5 internal diameter it is equal, up and down against, phase
Mutually perforation.
In conjunction with Fig. 1, Fig. 3, Fig. 4 and Fig. 8, the flash hole 3, level-one promotion part nozzle 6-3, missile wing 7, second level promotion part
The quantity of nozzle 13-4 and fire jetting hole 13-5 are 4, and 4 flash holes 3,4 level-one promotion part nozzle 6-3,4
A missile wing 7,4 second level promotion part nozzle 13-4 and 4 fire jetting hole 13-5 are respectively along the central axes of shell case 1 circumferentially formula array
Distribution.
In conjunction with Fig. 3 and Fig. 4, by the opposite of 1 inner wall of shell case and level-one promotion part outer wall 6-6 when 7 original state of missile wing
Against the missile wing 7, which compresses torsionspring 7-2 and buried, to be filled out inside shell case 1, in 1 He of shell case when 7 emission state of missile wing
After pinking portion 10 separates, is acted on by torsionspring 7-2 and being rotated counterclockwise along missile wing shaft 7-1, abut against 10 lower part of pinking portion
Screw thread 9 is sheared, continues to act on because of torsionspring 7-2 tension, constitutes 30 ° of constant subtended angles with the central axes in pinking portion 10.
As shown in fig. 6, the blast hole 10-5 is provided with 5 on the same axial direction in pinking portion 10, it is described same
5 blast hole 10-5 in axial direction constitute a blast hole group, and the quantity of the blast hole group is 8,8 blast hole groups
Central axes circumferentially formula array distribution along pinking portion 10.
As shown in figure 8, the oblique fumarole 14-3 is provided with 2 on the same axial direction in smoke portion 14, it is described
2 oblique fumarole 14-3 in same axial direction constitute an oblique fumarole group, and the quantity of the oblique fumarole group is 8
It is a, central axes circumferentially formula array distribution of the 8 oblique fumarole groups along smoke portion 14.
In conjunction with Fig. 7 and Figure 10, the pinking portion propagation squib relief hole 10-7-1 is to gather in the pinking portion side propagation squib 10-7
Aperture on wall, the tear-gas portion propagation squib radial direction relief hole 16-1-1 be gather it is small on tear-gas portion propagation squib 16-1 side wall
Hole, the tear-gas portion propagation squib axial direction relief hole 16-1-2 are the aperture to gather on tear-gas portion propagation squib 16-1 roof.
In the present embodiment, the phase Delay Tube 5, second level Delay Tube 8, three-level Delay Tube 11 and level Four Delay Tube 15
The extension time is respectively as follows: 1.5S, 3S, 2S and 2S, the phase Delay Tube 5, second level Delay Tube 8, three-level Delay Tube 11 and level Four
Delay Tube 15 is securely held at each Delay Tube jack by high-temperature plastic.
In conjunction with Fig. 1, Fig. 3, Fig. 6, Fig. 7, Fig. 8 and Figure 10, the flash hole 3, level-one promotion part nozzle 6-3, blast hole
10-5, pinking portion propagation squib relief hole 10-7-1, second level Delay Tube nozzle 13-4, fire jetting hole 13-5, oblique fumarole 14-3,
Tear-gas portion propagation squib radial direction relief hole 16-1-1 and tear-gas portion propagation squib axial direction relief hole 16-1-2 is sealed by hot melt adhesive.
Specific implementation step:
The present invention is inserted into the grenade launcher of corresponding bore, pulls the trigger of grenade launcher, firing pin hits mechanical
Impacting type fire in a stove before fuel is added 2-2, mechanical impact formula fire in a stove before fuel is added 2-2 are under fire and light the propellant powder 2-4 in the 2-3 of hyperbaric chamber, and propellant powder 2-4 is fierce
The a large amount of high temperature and pressure powder gases generated that burn enter low-pressure chamber 4 from flash hole 3, and the pressure in low-pressure chamber 4 is promoted to mention rapidly
It rises, push level-one promotion part 6 and forces the shearing screw thread 9 of connection pinking portion 10 and shell case 1 that failure by shear occurs, while level-one is prolonged
5 front of phase pipe is ignited, remaining body of pinking portion 10 and its connection continues to push under combustion gas effect, until the howitzer that flies out
The transmitting tube of transmitter, at this point, it is in 30 ° of subtended angles that missile wing 7, which under the action of torsionspring 7-2, opens, body continues to fly, and passes through
After the 1.5S extension time for crossing level-one Delay Tube 5, body flies out about 100 meters of transmitting tube, and 5 rear portion of level-one Delay Tube is under fire at this time,
The level-one promotion part propellant 6-2 in the propellant chamber 6-1 of level-one promotion part is lighted, propellant 6-2 burning in level-one promotion part generates
Combustion gas, the hot melt adhesive in the nozzle 6-3 of ablation level-one promotion part, combustion gas are realized from level-one promotion part nozzle 6-3 high speed ejection
Primary propulsion to body, while the front of second level Delay Tube 8 is ignited, after the extension of 3S, body flies second level Delay Tube 8
300 meters of row, 8 rear portion of second level Delay Tube is under fire, and lights the pinking portion booster 10-8 in pinking portion propagation squib 10-7, and pinking portion expands
Quick-fried medicine 10-8 fiercely burn generate powder gas sprayed out of pinking portion propagation squib relief hole 10-7-1, light glitter 10-6,
Broken pinking portion papery shell case 10-2 is fried in glitter 10-6 explosion, issues the strong deterrence sound from blast hole 10-5 and dazzles the eyes flash of light,
The front of three-level Delay Tube 11 is also ignited simultaneously, is delayed by 2S, and 100 meters of projectile flight, 11 rear portion of three-level Delay Tube is under fire,
Booster in the right booster box 12 of point, booster combustion explosion divide in pinking portion 10 and smoke portion 12 with second level promotion part 13
From the second level promotion part propellant 13-2 in the propellant chamber 13-1 of second level promotion part is ignited ignition, ablation second level promotion part tail
Hot melt adhesive in spout 13-4 and fire jetting hole 13-5, combustion gas are sprayed from second level promotion part nozzle 13-4, are realized to remaining body
Secondary propulsion, meanwhile, the smoke agent 14-2 in smoke-pot 14-1 is ignited, interference smog sprayed from oblique type fumarole 14-3,
Also can play progradation, remaining body continues 100 meters of flight, and the portion of smoke at this time 14 continues smoke, play the role of it is vast and hazy, in 2S
Delay after the time, the tear-gas portion booster 16-2 in tear-gas portion propagation squib 16-1 is ignited, and tear-gas portion booster 16-2 generates quick-fried
Fried release OC stimulates powder 16-4, and realizes the high speed lasing to rubber bullet 17-2.In entire emission process, projectile flight away from
From about 600 meters, successively realize that fright, smoke, tear-gas and kinetic energy hit multiple non-lethal action and efficacy, tactical qualities are diversified,
Conducive to the disposition of the sudden and violent riot of remote large-scale groups, also can be used for carrying out marine right-safeguarding law enforcement.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of variations, modification, replacement can be carried out to these embodiments without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (10)
1. the anti-riot howitzer of plural serial stage push type composite strike type, comprising: shell case (1), emission part (2), screw-in screw thread (2-
1), the mechanical impact formula fire in a stove before fuel is added (2-2), hyperbaric chamber (2-3), propellant powder (2-4), sealing cover foil (2-5), flash hole (3), low-pressure chamber
(4), level-one Delay Tube (5), level-one promotion part (6), level-one promotion part propellant chamber (6-1), level-one promotion part propellant (6-
2), level-one promotion part nozzle (6-3), level-one promotion part lower end Delay Tube jack (6-4), level-one promotion part upper end Delay Tube are inserted
Hole (6-5), level-one promotion part outer wall (6-6), missile wing (7), missile wing shaft (7-1), torsionspring (7-2), second level Delay Tube
(8), screw thread (9), pinking portion (10), pinking portion steel body (10-1), pinking portion papery shell case (10-2), pinking chamber are sheared
(10-3), pinking chamber lid (10-4), blast hole (10-5), glitter (10-6), pinking portion propagation squib (10-7), the expansion of pinking portion are quick-fried
Pipe relief hole (10-7-1), pinking portion booster (10-8), pinking portion bonding place (10-9), pinking subordinate end Delay Tube jack
(10-10), pinking portion upper end Delay Tube jack (10-11), three-level Delay Tube (11), booster box (12), second level promotion part
(13), second level promotion part propellant chamber (13-1), second level promotion part propellant (13-2), second level promotion part upper end Delay Tube jack
(13-3), second level promotion part nozzle (13-4), fire jetting hole (13-5), smoke portion (14), smoke-pot (14-1), smoke agent (14-
2), oblique fumarole (14-3), level Four Delay Tube (15), tear-gas portion (16), tear-gas portion propagation squib (16-1), tear-gas portion propagation squib
Radial relief hole (16-1-1), tear-gas portion propagation squib axial direction relief hole (16-1-2), tear-gas portion booster (16-2), tear-gas portion thorn
Swash powder chamber (16-3), OC stimulates powder (16-4), tear-gas subordinate end Delay Tube jack (16-5), kinetic energy portion (17), kinetic energy portion shell
Body (17-1), rubber bullet (17-2) and arch blast cap (17-3)；It is characterized by: the shell case (1) and pinking portion (10) are logical
Shearing screw thread (9) connection is crossed, the emission part (2) is set on shell case (1) lower end central axes, and the emission part (2) includes
Screw-in screw thread (2-1), the mechanical impact formula fire in a stove before fuel is added (2-2), hyperbaric chamber (2-3), propellant powder (2-4) and sealing cover foil (2-5), institute
It states emission part (2) and shell case (1) to be connected and fixed by screw-in screw thread (2-1), the mechanical impact formula fire in a stove before fuel is added (2-2) is riveted on
On emission part (2) bottom end central axes, hyperbaric chamber (2-3), the high pressure are provided on the upside of the mechanical impact formula fire in a stove before fuel is added (2-2)
Room (2-3) built-in propellant powder (2-4), the hyperbaric chamber (2-3) are sealed by sealing cover foil (2-5), on the sealing cover foil (2-5)
It is intensively provided with the pressure release aperture sealed by hot melt adhesive, the lower end surface of the emission part (2) and shell case (1) is evened up, the low pressure
Room (4) is connected to by flash hole (3) with hyperbaric chamber (2-3), is provided with one on the upside of shell case (1) upper inner, low-pressure chamber (4)
Grade promotion part (6), level-one promotion part (6) insertion are mounted on pinking portion (10) lower part, and the level-one promotion part (6) includes one
Grade promotion part propellant chamber (6-1), level-one promotion part propellant (6-2), level-one promotion part nozzle (6-3), level-one promotion part
Lower end Delay Tube jack (6-4), level-one promotion part upper end Delay Tube jack (6-5) and level-one promotion part outer wall (6-6), described one
Grade promotion part propellant chamber (6-1) built-in level-one promotion part propellant (6-2), under level-one promotion part propellant chamber (6-1)
End face is provided with level-one promotion part nozzle (6-3), and level-one promotion part lower end Delay Tube jack (6-4) is inserted with level-one extension
It manages (5), level-one promotion part upper end Delay Tube jack (6-5) is inserted with second level Delay Tube (8), before the level-one Delay Tube (5)
Portion is located at low-pressure chamber (4) inside, and level-one Delay Tube (5) rear portion is located at level-one promotion part propellant chamber (6-1) inside, described
It is provided with missile wing (7) on the outside of shell case (1) upper inner, level-one promotion part outer wall (6-6), the missile wing (7) includes missile wing shaft
(7-1) and torsionspring (7-2), level-one promotion part (6) upside are provided with pinking portion (10), and the pinking portion (10) includes
Pinking portion steel body (10-1), pinking portion papery shell case (10-2), pinking chamber (10-3), pinking chamber lid (10-4), blast hole
(10-5), glitter (10-6), pinking portion propagation squib (10-7), pinking portion booster (10-8), pinking portion bonding place (10-9),
Pinking subordinate end Delay Tube jack (10-10) and pinking portion upper end Delay Tube jack (10-11), the pinking portion steel body
Outside recess section is enclosed with pinking portion papery shell case (10-2) in the middle part of (10-1), the pinking portion papery shell case outer (10-2) with
The outer pinking portion steel body (10-1) is evened up, and is provided with pinking portion propagation squib (10-7) on pinking portion (10) central axes,
The built-in pinking portion booster (10-8) in pinking portion propagation squib (10-7) is arranged on the pinking portion propagation squib (10-7) tube wall
There is pinking portion propagation squib relief hole (10-7-1), is provided with pinking chamber (10-3), institute on the outside of pinking portion propagation squib (10-7)
It states pinking chamber (10-3) to be sealed by pinking chamber lid (10-4), the built-in glitter of the pinking chamber (10-3) (10-6), the pinking
Chamber (10-3) outer wall is provided with blast hole (10-5), and the pinking portion (10) is in pinking portion bonding place (10-9) and smoke portion (14)
Gluing is fixed, and pinking subordinate end Delay Tube jack (10-10) is inserted with the second stage of Delay Tube (8), and pinking portion upper end is delayed
Pipe jack (10-11) is inserted with three-level Delay Tube (11), and second phase Delay Tube (8) front is located at level-one promotion part propellant chamber
(6-1) is internal, and described second phase Delay Tube (8) rear portion is sequentially inserted into level-one promotion part upper end Delay Tube jack (6-5) and pinking portion
Lower end Delay Tube jack (10-10) is located at pinking portion propagation squib (10-7) inside afterwards, and three-level Delay Tube (11) front is located at
Pinking portion propagation squib (10-7) is internal, and three-level Delay Tube (11) rear portion is located at booster box (12) inside, the pinking portion
(10) upside be provided with second level promotion part (13), the second level promotion part (13) include second level promotion part propellant chamber (13-1),
Second level promotion part propellant (13-2), second level promotion part upper end Delay Tube jack (13-3), second level promotion part nozzle (13-4)
With fire jetting hole (13-5), the built-in second level promotion part propellant (13-2) in second level promotion part propellant chamber (13-1), described two
Grade promotion part upper end Delay Tube jack (13-3) is inserted with level Four Delay Tube (15), and second level promotion part (13) lower end surface is provided with
Second level promotion part nozzle (13-4), the fire jetting hole (13-5) is by second level promotion part propellant chamber (13-1) and smoke portion (14)
The cavity that connection, pinking portion (10) upper surface and second level promotion part (13) lower end surface are constituted is booster box (12), institute
Booster box (12) built-in booster is stated, is provided with smoke portion on the outside of pinking portion (10) upside, second level promotion part (13)
(14), the smoke portion (14) includes smoke-pot (14-1), smoke agent (14-2) and oblique fumarole (14-3), the smoke-pot
(14-1) is open circles cyclic structure, and smoke-pot (14-1) inside is against second level promotion part (13), the smoke-pot (14-
1) built-in smoke agent (14-2), smoke-pot (14-1) outside are provided with oblique fumarole (14-3), the second level promotion part
(13) upside is provided with tear-gas portion (16), and the tear-gas portion (16) includes tear-gas portion propagation squib (16-1), tear-gas portion booster
(16-2), tear-gas portion stimulate powder chamber (16-3), OC stimulation powder (16-4) and tear-gas subordinate end Delay Tube jack (16-5), described
Tear-gas portion propagation squib (16-1) is located on tear-gas portion (16) central axes, is provided with and urges on the tear-gas portion propagation squib (16-1) tube wall
Tear portion propagation squib radial direction relief hole (16-1-1) and tear-gas portion propagation squib axial direction relief hole (16-1-2), tear-gas portion propagation squib
(16-1) built-in tear-gas portion booster (16-2), tear-gas portion (16) outer wall constitutes tear-gas portion stimulation powder chamber (16-3), described
Tear-gas portion stimulates powder chamber (16-3) built-in OC stimulation powder (16-4), and tear-gas subordinate end Delay Tube jack (16-5) is inserted with four
Grade Delay Tube (15), the front of the level Four Delay Tube (15) are located inside second level promotion part propellant chamber (13-1), and described four
Grade Delay Tube (15) rear portion is sequentially inserted into second level promotion part upper end Delay Tube jack (13-3) and tear-gas subordinate end Delay Tube jack
(16-5) is located at tear-gas portion propagation squib (16-1) inside afterwards, is provided with kinetic energy portion (17) on the outside of the tear-gas portion (16), described dynamic
Energy portion (17) includes kinetic energy portion shell (17-1), rubber bullet (17-2) and arch blast cap (17-3), the rubber bullet (17-
It 2) is cannonball, the rubber bullet (17-2) is constituted in tear-gas portion stimulation powder chamber (16-3) and kinetic energy portion shell (17-1)
Close-packed arrays in space, the arch blast cap outer surface (17-3) are convex spherical shape structure, are conducive to reduce windage.
2. the anti-riot howitzer of plural serial stage push type composite strike type according to claim 1, it is characterised in that: the shell case
(1), screw-in screw thread (2-1), the mechanical impact formula fire in a stove before fuel is added (2-2), hyperbaric chamber (2-3), low-pressure chamber (4), level-one Delay Tube (5),
Level-one promotion part propellant chamber (6-1), level-one promotion part lower end Delay Tube jack (6-4), level-one promotion part upper end Delay Tube are inserted
Hole (6-5), second level Delay Tube (8), shearing screw thread (9), pinking portion steel body (10-1), pinking portion papery shell case (10-2),
It is pinking chamber (10-3), pinking chamber lid (10-4), pinking portion propagation squib (10-7), pinking subordinate end Delay Tube jack (10-10), quick-fried
Shake portion upper end Delay Tube jack (10-11), three-level Delay Tube (11), booster box (12), second level promotion part propellant chamber (13-
1), second level promotion part upper end Delay Tube jack (13-3), smoke-pot (14-1), level Four Delay Tube (15), tear-gas portion propagation squib
(16-1), tear-gas portion stimulate powder chamber (16-3), tear-gas subordinate end Delay Tube jack (16-5), kinetic energy portion shell (17-1) and arch
The central axes of blast cap (17-3) are overlapped, and level-one promotion part upper end Delay Tube jack (6-5) and pinking subordinate end Delay Tube are inserted
Hole (10-10) internal diameter is equal, up and down against, be mutually communicated, second level promotion part upper end Delay Tube jack (13-3) and tear-gas
Subordinate end Delay Tube jack (16-5) internal diameter is equal, up and down against, be mutually communicated.
3. the anti-riot howitzer of plural serial stage push type composite strike type according to claim 1, it is characterised in that: the biography fire
Hole (3), level-one promotion part nozzle (6-3), missile wing (7), second level promotion part nozzle (13-4) and fire jetting hole (13-5) number
Amount is 4, and 4 flash holes (3), 4 level-one promotion part nozzles (6-3), 4 missile wings (7), 4 second levels propulsions
Portion's nozzle (13-4) and 4 fire jetting holes (13-5) are respectively along the central axes of shell case (1) circumferentially formula array distribution.
4. the anti-riot howitzer of plural serial stage push type composite strike type according to claim 1, it is characterised in that: the missile wing
(7) by the opposite against missile wing (7) the compression torsion of shell case (1) inner wall and level-one promotion part outer wall (6-6) when original state
Spring (7-2) and being buried fill out it is internal in shell case (1), in shell case (1) and pinking portion (10) separation when missile wing (7) emission state
Afterwards, it is acted on by torsionspring (7-2) and being rotated counterclockwise along missile wing shaft (7-1), abut against the shearing spiral shell of pinking portion (10) lower part
Line (9) continues to act on because of torsionspring (7-2) tension, constitutes 30 ° of constant subtended angles with the central axes of pinking portion (10).
5. the anti-riot howitzer of plural serial stage push type composite strike type according to claim 1, it is characterised in that: the explosion
Hole (10-5) is provided with 5 on the same axial direction of pinking portion (10), 5 blast holes (10-5) in the same axial direction
A blast hole group is constituted, the quantity of the blast hole group is 8, central axes of the 8 blast hole groups along pinking portion (10)
Circumferentially formula array distribution.
6. the anti-riot howitzer of plural serial stage push type composite strike type according to claim 1, it is characterised in that: described oblique
Fumarole (14-3) is provided with 2 on the same axial direction of smoke portion (14), 2 oblique aerosol sprayings in the same axial direction
Hole (14-3) constitutes an oblique fumarole group, and the quantity of the oblique fumarole group is 8,8 oblique fumarole groups
Central axes circumferentially formula array distribution along smoke portion (14).
7. the anti-riot howitzer of plural serial stage push type composite strike type according to claim 1, it is characterised in that: the pinking
Portion's propagation squib relief hole (10-7-1) is the aperture to gather on pinking portion propagation squib (10-7) side wall, tear-gas portion propagation squib
Radial relief hole (16-1-1) is the aperture to gather on tear-gas portion propagation squib (16-1) side wall, and tear-gas portion propagation squib is axial
Relief hole (16-1-2) is the aperture to gather on tear-gas portion propagation squib (16-1) roof.
8. the anti-riot howitzer of plural serial stage push type composite strike type according to claim 1, it is characterised in that: the phase
Delay Tube (5), second level Delay Tube (8), three-level Delay Tube (11) and level Four Delay Tube (15) the extension time be respectively as follows: 1.5S,
3S, 2S and 2S, the phase Delay Tube (5), second level Delay Tube (8), three-level Delay Tube (11) and level Four Delay Tube (15) pass through
High-temperature plastic is securely held at each Delay Tube jack.
9. the anti-riot howitzer of plural serial stage push type composite strike type according to claim 1, it is characterised in that: the biography fire
Hole (3), level-one promotion part nozzle (6-3), blast hole (10-5), pinking portion propagation squib relief hole (10-7-1), second level are delayed
Pipe nozzle (13-4), fire jetting hole (13-5), oblique fumarole (14-3), tear-gas portion propagation squib radial direction relief hole (16-1-1) and
Tear-gas portion propagation squib axial direction relief hole (16-1-2) is sealed by hot melt adhesive.
10. the anti-riot howitzer of plural serial stage push type composite strike type according to claim 1, it is characterised in that: the bullet
Shell (1) is by aluminum alloy materials processing and fabricating, and tear-gas portion stimulation powder chamber (16-3) cavity wall and kinetic energy portion shell (17-1) are by PVC
Material processing and fabricating.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811654994.3A CN109596009B (en) | 2018-12-27 | 2018-12-27 | Multistage series pushing type composite striking type riot grenade |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811654994.3A CN109596009B (en) | 2018-12-27 | 2018-12-27 | Multistage series pushing type composite striking type riot grenade |
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| CN109596009A true CN109596009A (en) | 2019-04-09 |
| CN109596009B CN109596009B (en) | 2024-03-08 |
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|---|---|---|---|
| CN201811654994.3A Active CN109596009B (en) | 2018-12-27 | 2018-12-27 | Multistage series pushing type composite striking type riot grenade |
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| CN111765814A (en) * | 2020-07-10 | 2020-10-13 | 中国人民武装警察部队工程大学 | Compound anti-riot kinetic energy bullet with two-stage dissipation mechanism |
| CN113513949A (en) * | 2021-07-22 | 2021-10-19 | 北京理工大学 | Single-stage type energy-collecting charging structure capable of forming explosion-penetrating time sequence combined action |
| CN113587736A (en) * | 2021-08-25 | 2021-11-02 | 中国人民武装警察部队工程大学 | Composite anti-riot kinetic energy bullet with delay boosting function |
| US20220099419A1 (en) * | 2018-06-14 | 2022-03-31 | Liberty Dynamic, Llc | Chemical agent delivery receptacle with reusable digital control cartridge |
| CN115281176A (en) * | 2022-07-11 | 2022-11-04 | 徐爱春 | Throw formula device through reputation flavor drives from wild brown bear |
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| CN109596009B (en) | 2024-03-08 |
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