CN102371040B - High-temperature sensing fire-fighting rocket bomb - Google Patents
High-temperature sensing fire-fighting rocket bomb Download PDFInfo
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- CN102371040B CN102371040B CN 201010253689 CN201010253689A CN102371040B CN 102371040 B CN102371040 B CN 102371040B CN 201010253689 CN201010253689 CN 201010253689 CN 201010253689 A CN201010253689 A CN 201010253689A CN 102371040 B CN102371040 B CN 102371040B
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- temperature sensing
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- Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
Abstract
The invention relates to a high-temperature sensing fire-fighting rocket bomb which is especially suitable to be used for carrying out fire extinguishing on high-risk fire scenes such as forests, oil storage tanks, high-rise buildings and the like to which firefighters can not be close. The high-temperature sensing fire-fighting rocket bomb is structurally characterized in that a high-temperature sensor fixed on the top of a bomb head is sequentially connected with a temperature controller, a power switch, a battery pack and a transformer arranged in the bomb, two sets of positive and negative electrode slabs (connected with the transformer) and explosives are arranged in a narrow tube of the bomb body, the bomb head end of the bomb body is provided with a sealed tube and a liquid injection tube, a water-based fire-extinguishing agent is filled in the cavity of the bomb body, and a thruster is fixedly inserted in the tail part of the bomb body. The high-temperature sensing fire-fighting rocket bomb provided by the invention can be launched by a civilian helicopter or through vehicle-mounted launching, and through high-temperature sensing and self-dependent detonating, a large number of the water-based fire-extinguishing agent carried by the rocket bomb is directly sprayed on the surfaces of comburents, therefore, the fire extinguishing effect is good; and because the rocket bomb is provided with the thruster, the rocket bomb can achieve an effect of long-range launching without topographical and traffic restrictions, and can be exactly hit to the inside of a fire point, thereby achieving the purposes of rapid and safe fire extinguishing and casualties reduction.
Description
Technical field the present invention relates to is a kind of high temperature induction fire-fighting rocket bomb that is particularly suitable for the scene of a fire fire extinguishing use as high-risk, high-leveled and difficult in forest, oil port, oil storage tank, warehouse, chemical plant, skyscraper etc. that the fire fighter can not be close.
Background technology has multitube emission and spin fire-fighting rocket bomb technology in the prior art, because the cost of multitube emission fire-fighting rocket bomb is higher, implements certain difficulty; And the extinguishing chemical of self-rotary fire-fighting rocket bomb is evenly spilling of a little, so speed and the effect of fire extinguishing are not very good.
Summary of the invention reduces the cost of fire-fighting rocket bomb for overcoming above shortcomings in prior art, improves speed and the effect of quick extinguishing, the invention provides a kind of high temperature induction fire-fighting rocket bomb.the design of high temperature of the present invention induction fire-fighting rocket bomb is: be fixed with the high temperature inductor at conical bullet top, in the bullet with heat-insulation plate with inner lining, be provided with the temperature controller that is being connected successively by wire with the high temperature inductor, power switch, batteries, transformer, be provided with a tubule on the afterbody compartment in the holder of annular protrusion in the tubulose body that is connected with bullet, just be equipped be connected with transformer two groups in tubule, negative electrode piece and explosive, on body bullet one end end socket, the centre position of tubule is provided with wears the sealed tube that wire is used, side at tubule is provided with liquid injection pipe, be marked with the aqua type extinguishing chemical in the cavity of body, pass through the afterbody open slot interpolation set of afterbody compartment formation by shell at body, the shell afterbody is provided with fixing electronic telecontrol igniter, and the propeller that in shell, the gunpowder propellant that is equipped with consists of.High temperature induction fire-fighting rocket bomb of the present invention is different from existing fire extinguisher bomb, and it can adopt civil helicopter or vehicle-mounted radiation pattern, and the delivery emission is convenient.This rocket projectile adopts temperature sense control system, in the time of in bullet is squeezed into the scene of a fire, independently ignites in the 500-1500 Celsius temperature, and a large amount of aqua type extinguishing chemicals in rocket projectile are sprayed directly on comburant surface, good extinguishing effect.With propeller, so can realize long-range emission, can accurately get to the inside of fire point because of this rocket projectile self, reach quick, safe fire extinction, reduce the casualties purpose.Because can long-rangely launch, so be not subjected to the restriction of landform, traffic, the putting out a fire to save life and property of as high-risk in forest, oil port, oil storage tank, warehouse, chemical plant, skyscraper etc., the high-leveled and difficult scene of a fire that is particularly useful for that the fire fighter can't be close.
Appended drawings is the structural representation of high temperature induction fire-fighting rocket bomb of the present invention.
The specific embodiment is in order to have further understanding to structure of the present invention and principle, and details are as follows by reference to the accompanying drawings:
with reference to accompanying drawing, the structure of high temperature induction fire-fighting rocket bomb of the present invention is, at conical bullet 1 top, three high temperature inductors 3 are housed fixedly, in the bullet 1 with heat-insulation plate with inner lining 8, be provided with the temperature controller 4 that is connected successively by wire with high temperature inductor 3, power switch 7, batteries 5, transformer 6, interleave an intrinsic tubule 9 in the holder of annular protrusion on the interior afterbody compartment of body 2 of the tubulose that is being connected by screw with bullet 1, just be equipped be connected with transformer 6 by wire two groups in tubule 9, negative electrode piece 10 and explosive 11, on the end socket of bullet one end of body 2, be provided with on the position of the centre of tubule 9 and wear the sealed tube 12 that wire is used, be provided with the liquid injection pipe 13 of injected water fundamental mode extinguishing chemical 14 in body 2 cavitys on the end socket position of tubule 9 sides, pass through the afterbody open slot interpolation set of afterbody compartment formation by shell 15 at body 2, shell 15 afterbodys are provided with fixing electronic telecontrol igniter 16, and the propeller that in shell 15, the gunpowder propellant 17 that is equipped with consists of.Bullet 1 in this rocket projectile, body 2 and angle of rake shell 15 all adopt the composite glass fiber reinforced making of macromolecule.
its principle is: when external environment reaches certain temperature, namely when this rocket projectile is launched in the scene of a fire, under the high temperature action of flame, high temperature inductor 3 and temperature controller 4 control transformers 6 produce powerful electric current, two groups by entering that sealed tube 12 inside conductors connect just, negative electrode plate 8 produces powerful electric arc, thereby the explosive 11 of igniting in body 2 inner tubules 9 produces blast, body 2 is blown, the shock wave that blast produces can spill the body surface that is burning to surrounding to the entrained aqua type extinguishing chemical 14 of rocket projectile and intercept air, reduce the temperature of comburant, and then the control intensity of a fire, reach the purpose of quick extinguishing.First power switch 7 is opened before emission.
Claims (2)
1. a high temperature is responded to fire-fighting rocket bomb, it is characterized in that being fixed with high temperature inductor (3) at conical bullet (1) top, in the bullet (1) with heat-insulation plate with inner lining (8), be provided with the temperature controller (4) that is being connected successively by wire with high temperature inductor (3), power switch (7), batteries (5), transformer (6), be provided with a tubule (9) in the holder of annular protrusion on the interior afterbody compartment of body (2) of the tubulose that is connected with bullet (1), just be equipped be connected with transformer (6) two groups in tubule (9), negative electrode piece (10) and explosive (11), on body (2) bullet one end end socket, be provided with the sealed tube (12) of wearing wire and using on the centre position of tubule (9), be provided with liquid injection pipe (13) in the side of tubule (9), be marked with aqua type extinguishing chemical (14) in the cavity of body (2), pass through the afterbody open slot interpolation set of afterbody compartment formation by shell (15) at body (2), shell (15) afterbody is provided with fixing electronic telecontrol igniter (16), and the propeller that in shell (15), the gunpowder propellant (17) that is equipped with consists of, bullet (1), it is composite glass fiber reinforced that body (2) and angle of rake shell (15) are macromolecule.
2. high temperature induction fire-fighting rocket bomb according to claim 1, is characterized in that there are three at the fixing high temperature inductor (3) in conical bullet (1) top.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201010253689 CN102371040B (en) | 2010-08-09 | 2010-08-09 | High-temperature sensing fire-fighting rocket bomb |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201010253689 CN102371040B (en) | 2010-08-09 | 2010-08-09 | High-temperature sensing fire-fighting rocket bomb |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN102371040A CN102371040A (en) | 2012-03-14 |
| CN102371040B true CN102371040B (en) | 2013-05-08 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201010253689 Expired - Fee Related CN102371040B (en) | 2010-08-09 | 2010-08-09 | High-temperature sensing fire-fighting rocket bomb |
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| Country | Link |
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| CN (1) | CN102371040B (en) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103751929B (en) * | 2014-01-17 | 2017-01-11 | 吴玉臣 | Remote rapid fire extinguishing device |
| CN103884244A (en) * | 2014-04-11 | 2014-06-25 | 成都理工大学 | Blasting warhead with mechanical delay fuze |
| CN105749458A (en) * | 2014-12-18 | 2016-07-13 | 常熟市福安消防设备有限公司 | Throwing-type fire-fighting fire-extinguishing bomb |
| CN106890413A (en) * | 2017-04-28 | 2017-06-27 | 成都谍翼科技有限公司 | Fire-fighting rocket projectile and fire-fighting system |
| CN207734492U (en) * | 2017-12-11 | 2018-08-17 | 陈春霞 | Fire extinguisher bomb and its emission system |
| CN111569314B (en) * | 2020-05-30 | 2021-07-30 | 山东同其数字技术有限公司 | Forest fire-extinguishing missile |
| CN113048847A (en) * | 2021-03-23 | 2021-06-29 | 哈尔滨工程大学 | Gradient type uniform detonation center booster based on multiple ignition positions |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101130133A (en) * | 2007-09-30 | 2008-02-27 | 杨国俊 | Remote multi-tube extinguishment launcher and extinguishment rocket ammunition system thereof |
| CN101703830A (en) * | 2009-11-09 | 2010-05-12 | 哈尔滨工程大学 | Pneumatic emission-type forest extinguishing cannonball |
| CN201735102U (en) * | 2010-08-09 | 2011-02-09 | 赵义刚 | High-temperature sensing type fire fighting rocket-powered missile |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE10346163A1 (en) * | 2003-10-04 | 2005-05-04 | Diehl Bgt Defence Gmbh & Co Kg | Missile for fire fighting |
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2010
- 2010-08-09 CN CN 201010253689 patent/CN102371040B/en not_active Expired - Fee Related
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101130133A (en) * | 2007-09-30 | 2008-02-27 | 杨国俊 | Remote multi-tube extinguishment launcher and extinguishment rocket ammunition system thereof |
| CN101703830A (en) * | 2009-11-09 | 2010-05-12 | 哈尔滨工程大学 | Pneumatic emission-type forest extinguishing cannonball |
| CN201735102U (en) * | 2010-08-09 | 2011-02-09 | 赵义刚 | High-temperature sensing type fire fighting rocket-powered missile |
Also Published As
| Publication number | Publication date |
|---|---|
| CN102371040A (en) | 2012-03-14 |
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