CN109115053A - Individual soldier's incendiary rocket - Google Patents
Individual soldier's incendiary rocket Download PDFInfo
- Publication number
- CN109115053A CN109115053A CN201810959162.6A CN201810959162A CN109115053A CN 109115053 A CN109115053 A CN 109115053A CN 201810959162 A CN201810959162 A CN 201810959162A CN 109115053 A CN109115053 A CN 109115053A
- Authority
- CN
- China
- Prior art keywords
- shell
- booster
- shield
- head
- incendiary
- 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.)
- Pending
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Classifications
-
- 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
-
- 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
- F42B10/04—Stabilising arrangements using fixed fins
- F42B10/06—Tail fins
- F42B10/08—Flechette-type projectiles
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The invention discloses a kind of individual soldier's incendiary rockets, including fuse, head-shield, shell, booster and incendiary agent, the fuse is fixedly connected with the front end of the head-shield, the rear end of the head-shield is fixedly connected with the front end of the shell, the booster is fixed in the shell, and the booster is ignited end and is connect with the ignition end of the fuse, the incendiary agent is fixed between the lateral surface of the booster and the medial surface of the shell, and the rear end of the shell is fixedly connected with empennage.Using domestic active service, pickaback Individual Rocket Launching Tube emits individual soldier's incendiary rocket to dead angle to a kind of individual soldier's incendiary rocket of the present invention, explosive combustion, form large range of high-temperature area, burning strike is implemented to dead angle target, and incendiary agent weight is greater than similar product, have the characteristics that burning time is long, ignition temperature is high, burning area is big, it is significant to the strike effect of dead angle target.
Description
Technical field
The present invention relates to artillery field more particularly to a kind of individual soldier's incendiary rockets.
Background technique
Terrorist forces tend to be active in recent years, mostly using key city as target.It is terrified in the fight-terrorism warfare of city
Molecule is screened by complicated city massive construction environment, is usually hidden at dead angle, existing weaponry and equipment is difficult to play
Effect.Currently, burning of setting on fire is the effective means for tackling dead angle target.Existing individual soldier's incendiary weapon mainly has: flame projector and list
Soldier's incendiary projectile (such as China DFR89 formula 36mm individual soldier firebomb and FHJ01 formula individual soldier firebomb).Effective operational distance of flame projector
Generally within 60m, and operation team member exposure is excessive when flame, vulnerable to attack, is not suitable for urban environment and uses.Individual soldier is vertical
The incendiary agent weight of fiery bullet filling is too small, and combustion efficiency is not significant, is mainly used for field operation and sets on fire shielding.
To solve in urban operation to the remote Percussion Problems of dead angle target, the present invention is with domestic active service pickaback individual soldier
Rocket launcher is flat pad, proposes a kind of individual soldier's incendiary rocket, can be obviously improved to hiding in urban operation in dead angle target
Striking capabilities, will effectively promote anti-terrorism equipment Development.
Summary of the invention
The object of the invention is that providing a kind of individual soldier's incendiary rocket to solve the above-mentioned problems.
The present invention through the following technical solutions to achieve the above objectives:
A kind of individual soldier's incendiary rocket, including fuse, head-shield, shell, booster and incendiary agent, the fuse and the head-shield
Front end be fixedly connected, the rear end of the head-shield is fixedly connected with the front end of the shell, and the booster is fixed at described
In shell, and the booster is ignited end and is connect with the ignition end of the fuse, and the incendiary agent is fixed at the booster
Between lateral surface and the medial surface of the shell, the rear end of the shell is fixedly connected with empennage.
Specifically, the fuse is ladder revolving structure, and the rear end of the fuse is miner diameter end；
The head-shield is ladder-like hollow revolving structure, and the front end of the head-shield is miner diameter end, and the rear end of the head-shield is
Bigger diameter end is connected between the front end of the head-shield and the rear end of the head-shield by arc surface transition；
The shell is ladder-like hollow revolving structure, and the front end of the shell is bigger diameter end, and the rear end of the shell is
Miner diameter end is connected between the front end of the shell and the rear end of the shell by arc surface transition；
The miner diameter end of the fuse is arranged in the miner diameter end of the head-shield, and is threadably secured connection, the shell
Bigger diameter end be arranged in the bigger diameter end of the head-shield, and be threadably secured connection.
Specifically, the booster is ladder-like hollow revolving structure, and the front end of the booster is bigger diameter end, the booster
Rear end is miner diameter end, and the booster and the shell are coaxially disposed, the lateral surface of the bigger diameter end of the booster and the shell
The medial surface of bigger diameter end is threadably secured connection, is arranged between the path section of the booster and the medial surface of the shell free
Chamber, the incendiary agent are fixed in the cavity.
Specifically, the empennage is blade type thin slice, and the rear end lateral surface of the shell is provided with mounting groove, the empennage
Root is provided with installation circular hole, and the root of the empennage is arranged in the mounting groove and by passing through inserting for the installation circular hole
Pin is fixedly connected with the shell.
Preferably, the quantity of the empennage is four.
Preferably, the fuse is impact fuze, and the incendiary agent is solidified gasoline.
The beneficial effects of the present invention are:
A kind of individual soldier's incendiary rocket of the present invention using domestic active service pickaback Individual Rocket Launching Tube by individual soldier's incendiary rocket
Near transmitting to dead angle, explosive combustion forms large range of high-temperature area, implements burning strike to dead angle target, and fire
It burns agent weight and is greater than similar product, have the characteristics that burning time is long, ignition temperature is high, burning area is big, dead angle target is beaten
Hit significant effect.
Detailed description of the invention
Fig. 1 is individual soldier's incendiary rocket structural schematic diagram of the present invention；
Fig. 2 is the structural schematic diagram of fuse of the present invention；
Fig. 3 is the structural schematic diagram of head-shield of the present invention；
Fig. 4 is the structural schematic diagram of shell of the present invention；
Fig. 5 is the structural schematic diagram of booster of the present invention；
Fig. 6 is the structural schematic diagram of empennage of the present invention.
Specific embodiment
The present invention will be further explained below with reference to the attached drawings:
As shown in Figure 1, a kind of individual soldier's incendiary rocket of the present invention, including fuse 1, head-shield 2, shell 4, booster 3 and burning
Agent 5, fuse 1 are fixedly connected with the front end of head-shield 2, and the rear end of head-shield 2 is fixedly connected with the front end of shell 4, and booster 3 is fixedly installed
In shell 4, and booster 3 is ignited end and is connect with the ignition end of fuse 1, and incendiary agent 5 is fixed at the lateral surface and shell of booster 3
Between the medial surface of body 4, the rear end of shell 4 is fixedly connected with empennage 6.
As shown in Fig. 2, fuse 1 is stairstepping rotary structure, the miner diameter end of the outer diameter of the miner diameter end of fuse 1 with head-shield 2
The aperture of internal thread hole, and the external peripheral surface of the miner diameter end of fuse 1 has connection external screw thread, and fuse 1 is impact fuze 1.
As shown in figure 3, head-shield 2 is ladder-like hollow rotary structure, the miner diameter end and bigger diameter end of head-shield 2 are to wait wall thickness
Cylindrical structure, the bigger diameter end and miner diameter end of head-shield 2 are arc surface transition.The bigger diameter end and miner diameter end of head-shield 2 have one section have in
Isometrical section of screw thread, the aperture of the miner diameter end internal thread hole of head-shield 2 are equal to the outer diameter of the miner diameter end of fuse 1, the miner diameter end of head-shield 2
It is connected through a screw thread with the miner diameter end of fuse 1.
As shown in figure 4, shell 4 is ladder-like hollow rotary structure, the bigger diameter end of shell 4 is to wait wall thickness cylindrical structure,
The bigger diameter end and miner diameter end of shell 4 are arc surface transition.The bigger diameter end outer diameter of shell 4 is equal to the internal screw thread of the bigger diameter end of head-shield 2
The aperture in hole, and the external peripheral surface of the bigger diameter end of shell 4 has connection screw thread, the bigger diameter end outer round surface and head-shield 2 of shell 4
Connection, the aperture of the internal thread hole of the bigger diameter end of head-shield 2 are equal to the outer diameter of the bigger diameter end of shell 4, the bigger diameter end and shell of head-shield 2
4 bigger diameter end is connected through a screw thread.
As shown in figure 5, booster 3 is ladder-like hollow rotary structure, the bigger diameter end and miner diameter end of booster 3 are to wait wall thickness
Cylindrical structure, the outer diameter of the bigger diameter end of booster 3 are equal to the aperture of the bigger diameter end internal thread hole of shell 4, the bigger diameter end of booster 3 it is outer
Circumferential surface has connection external screw thread, and the bigger diameter end internal diameter of shell 4 is equal to the aperture of 3 larger diameter end outside threaded holes of booster, shell 4
The inner circumferential surface of bigger diameter end has connection internal screw thread, and the bigger diameter end inner headed face of shell 4 is threadedly coupled with the bigger diameter end of booster 3.
Booster 3 and shell 4 are coaxially disposed, and are provided with cavity between the path section of booster 3 and the medial surface of shell 4, are burnt
Agent 5 is fixed in cavity, and incendiary agent 5 is solidified gasoline.
As shown in fig. 6, empennage 6 is blade type thin slice, there is installation circular hole in 6 root of empennage, and the miner diameter end outer round surface of shell 4 has
Mounting groove, installation slot number are 4, and empennage 6 assigns into mounting groove, 6 quantity of empennage 4.
In use, by domestic active service, pickaback Individual Rocket Launching Tube is by rocket bomb transmitting, when the fuse 1 of the front end of rocket projectile
It after being impacted, ignites and booster 3 is made to explode, booster 3 ignites the incendiary agent 5 in 3 outside of booster after exploding, while in the work of explosion
Under firmly, incendiary agent 5 scatter, and realizes the purpose of dead angle strike.
Above-described embodiment is presently preferred embodiments of the present invention, is not a limitation on the technical scheme of the present invention, as long as
Without the technical solution that creative work can be realized on the basis of the above embodiments, it is regarded as falling into the invention patent
Rights protection scope in.
Claims (6)
1. a kind of individual soldier's incendiary rocket, it is characterised in that: including fuse, head-shield, shell, booster and incendiary agent, the fuse
It is fixedly connected with the front end of the head-shield, the rear end of the head-shield is fixedly connected with the front end of the shell, and the booster is fixed
It is arranged in the shell, and the booster is ignited end and connect with the ignition end of the fuse, the incendiary agent is fixed at
Between the lateral surface of the booster and the medial surface of the shell, the rear end of the shell is fixedly connected with empennage.
2. individual soldier's incendiary rocket according to claim 1, it is characterised in that: the fuse is ladder revolving structure, institute
The rear end for stating fuse is miner diameter end；
The head-shield is ladder-like hollow revolving structure, and the front end of the head-shield is miner diameter end, and the rear end of the head-shield is major diameter
End, is connected between the front end of the head-shield and the rear end of the head-shield by arc surface transition；
The shell is ladder-like hollow revolving structure, and the front end of the shell is bigger diameter end, and the rear end of the shell is path
End, is connected between the front end of the shell and the rear end of the shell by arc surface transition；
The miner diameter end of the fuse is arranged in the miner diameter end of the head-shield, and is threadably secured connection, the shell it is big
Diameter end is arranged in the bigger diameter end of the head-shield, and is threadably secured connection.
3. individual soldier's incendiary rocket according to claim 2, it is characterised in that: the booster is ladder-like hollow revolution knot
Structure, the front end of the booster are bigger diameter end, and the rear end of the booster is miner diameter end, and the booster and the shell are coaxially disposed,
The lateral surface of the bigger diameter end of the booster is threadably secured with the medial surface of the bigger diameter end of the shell and connect, the booster
Cavity is provided between path section and the medial surface of the shell, the incendiary agent is fixed in the cavity.
4. individual soldier's incendiary rocket according to claim 2, it is characterised in that: the empennage is blade type thin slice, the shell
The rear end lateral surface of body is provided with mounting groove, and the root of the empennage is provided with installation circular hole, and the root setting of the empennage exists
In the mounting groove and the bolt by passing through the installation circular hole is fixedly connected with the shell.
5. individual soldier's incendiary rocket according to claim 4, it is characterised in that: the quantity of the empennage is four.
6. individual soldier's incendiary rocket according to claim 1, it is characterised in that: the fuse is impact fuze, the combustion
Burning agent is solidified gasoline.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810959162.6A CN109115053A (en) | 2018-08-22 | 2018-08-22 | Individual soldier's incendiary rocket |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810959162.6A CN109115053A (en) | 2018-08-22 | 2018-08-22 | Individual soldier's incendiary rocket |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109115053A true CN109115053A (en) | 2019-01-01 |
Family
ID=64852769
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810959162.6A Pending CN109115053A (en) | 2018-08-22 | 2018-08-22 | Individual soldier's incendiary rocket |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109115053A (en) |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB250271A (en) * | 1925-04-06 | 1926-10-21 | Skoda Works Ltd Company | Improvements in aerial bombs |
| GB259539A (en) * | 1925-10-12 | 1927-07-21 | Bohdan Pantoflicek | Improvements in or relating to bombs or the like |
| GB1245906A (en) * | 1969-01-20 | 1971-09-15 | Bofors Ab | Explosive shell |
| RU2082943C1 (en) * | 1994-01-25 | 1997-06-27 | Владимир Алексеевич Одинцов | High-explosive rocket projectile |
| US6276277B1 (en) * | 1999-04-22 | 2001-08-21 | Lockheed Martin Corporation | Rocket-boosted guided hard target penetrator |
| RU2291378C1 (en) * | 2005-08-29 | 2007-01-10 | Федеральное Государственное унитарное предприятие "Государственное научно-производственное предприятие "Сплав" | Jet projectile |
| US20120227609A1 (en) * | 2010-07-29 | 2012-09-13 | Alliant Techsystems Inc. | Initiation systems for explosive devices, scalable output explosive devices including initiation systems, and related methods |
| CN105435398A (en) * | 2014-09-26 | 2016-03-30 | 沈阳理工大学 | Individual-soldier portable equilibrium emission type high-rise building fire extinguishing bomb |
| CN208688344U (en) * | 2018-08-22 | 2019-04-02 | 中国工程物理研究院总体工程研究所 | Individual soldier's incendiary rocket |
-
2018
- 2018-08-22 CN CN201810959162.6A patent/CN109115053A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB250271A (en) * | 1925-04-06 | 1926-10-21 | Skoda Works Ltd Company | Improvements in aerial bombs |
| GB259539A (en) * | 1925-10-12 | 1927-07-21 | Bohdan Pantoflicek | Improvements in or relating to bombs or the like |
| GB1245906A (en) * | 1969-01-20 | 1971-09-15 | Bofors Ab | Explosive shell |
| RU2082943C1 (en) * | 1994-01-25 | 1997-06-27 | Владимир Алексеевич Одинцов | High-explosive rocket projectile |
| US6276277B1 (en) * | 1999-04-22 | 2001-08-21 | Lockheed Martin Corporation | Rocket-boosted guided hard target penetrator |
| RU2291378C1 (en) * | 2005-08-29 | 2007-01-10 | Федеральное Государственное унитарное предприятие "Государственное научно-производственное предприятие "Сплав" | Jet projectile |
| US20120227609A1 (en) * | 2010-07-29 | 2012-09-13 | Alliant Techsystems Inc. | Initiation systems for explosive devices, scalable output explosive devices including initiation systems, and related methods |
| CN105435398A (en) * | 2014-09-26 | 2016-03-30 | 沈阳理工大学 | Individual-soldier portable equilibrium emission type high-rise building fire extinguishing bomb |
| CN208688344U (en) * | 2018-08-22 | 2019-04-02 | 中国工程物理研究院总体工程研究所 | Individual soldier's incendiary rocket |
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