CN106267637A - UAV system fire extinguisher bomb - Google Patents
UAV system fire extinguisher bomb Download PDFInfo
- Publication number
- CN106267637A CN106267637A CN201610892816.9A CN201610892816A CN106267637A CN 106267637 A CN106267637 A CN 106267637A CN 201610892816 A CN201610892816 A CN 201610892816A CN 106267637 A CN106267637 A CN 106267637A
- Authority
- CN
- China
- Prior art keywords
- stay tube
- fixing
- fire extinguisher
- igniter
- extinguisher bomb
- 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.)
- Granted
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Classifications
-
- A—HUMAN NECESSITIES
- A62—LIFE-SAVING; FIRE-FIGHTING
- A62C—FIRE-FIGHTING
- A62C19/00—Hand fire-extinguishers in which the extinguishing substance is expelled by an explosion; Exploding containers thrown into the fire
-
- A—HUMAN NECESSITIES
- A62—LIFE-SAVING; FIRE-FIGHTING
- A62C—FIRE-FIGHTING
- A62C3/00—Fire prevention, containment or extinguishing specially adapted for particular objects or places
- A62C3/02—Fire prevention, containment or extinguishing specially adapted for particular objects or places for area conflagrations, e.g. forest fires, subterranean fires
- A62C3/0214—Fire prevention, containment or extinguishing specially adapted for particular objects or places for area conflagrations, e.g. forest fires, subterranean fires for buildings or installations in fire storms
-
- A—HUMAN NECESSITIES
- A62—LIFE-SAVING; FIRE-FIGHTING
- A62C—FIRE-FIGHTING
- A62C3/00—Fire prevention, containment or extinguishing specially adapted for particular objects or places
- A62C3/02—Fire prevention, containment or extinguishing specially adapted for particular objects or places for area conflagrations, e.g. forest fires, subterranean fires
- A62C3/0228—Fire prevention, containment or extinguishing specially adapted for particular objects or places for area conflagrations, e.g. forest fires, subterranean fires with delivery of fire extinguishing material by air or aircraft
- A62C3/025—Fire extinguishing bombs; Projectiles and launchers therefor
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02A—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
- Y02A40/00—Adaptation technologies in agriculture, forestry, livestock or agroalimentary production
- Y02A40/10—Adaptation technologies in agriculture, forestry, livestock or agroalimentary production in agriculture
- Y02A40/28—Adaptation technologies in agriculture, forestry, livestock or agroalimentary production in agriculture specially adapted for farming
Landscapes
- Health & Medical Sciences (AREA)
- Public Health (AREA)
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Life Sciences & Earth Sciences (AREA)
- Biodiversity & Conservation Biology (AREA)
- Ecology (AREA)
- Forests & Forestry (AREA)
- Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
nullThe present invention relates to a kind of UAV system fire extinguisher bomb，Including taper bullet、Electronic compartment、Body、Rear end cap、Inner cone bar、Rear cone bar、Prop up stay tube、Igniter、Electromotor、Saucisson and anti-light interference infrared sensor，Described taper bullet is fixing with one end of inner cone bar to be connected，Electronic compartment is fixing with one end of body to be connected，Rear end cap is fixing with the other end of body to be connected，Prop up stay tube and be positioned at body，The other end of inner cone bar is fixing with stay tube one end to be connected，Rear cone bar is fixing with a stay tube other end and rear end cap to be connected，Described electromotor is fixing with rear end cap to be connected，It is provided with saucisson in described stay tube，Gunpowder it is provided with in saucisson，Prop up and between stay tube and body, be provided with firing-fighting medium，Igniter is positioned at electronic compartment，And the ignition fuse of igniter stretches in saucisson，And anti-light interference infrared sensor electrically connects with the wiring board of igniter.The present invention can bear the impulsive force crashing through glass, effectively protects firing-fighting medium, improves extinguishing effect.
Description
Technical field
The present invention relates to a kind of fire-extinguishing apparatus, especially a kind of UAV system fire extinguisher bomb.
Background technology
Along with socioeconomic fast development, living standards of the people improve constantly, and high-rise building building will progressively replace many
Floor room becomes the main building of city-building.The development of high-rise building construction decreases floor space, has saved space, simultaneously
Also new requirement is highlighted for security against fire lifesaving system.Although to security against fire in the design, building course of high-rise building
It is proposed strict requirements, but still suffers from deficiency in the ability tackling urgent accident.
Affected by operation principle and physics limit, for the special type fire control vehicle of more than hundred meters high-rise building external rescues
Equipment generally exists that car body is roomy, developed area big, supply and the feature such as Support Equipment is complicated, thus brings many existing by rescue
Field limits, and rescues and Support Equipment " enters and do not goes ", " Zhan Bukai ", the application problem of " can't reach ", have impact on rescue outfit
The performance of energy.
Therefore fire extinguisher bomb is arisen spontaneously, and traditional fire extinguisher bomb typically uses kraft paper or Reinforced foam material, blows rear wink
Between be just powder, human body will not be damaged.But impact and the extruding force crashing through glass is born with kraft paper shell, can be right
Body damages, and affects extinguishing effect, even cannot put out a fire.
Summary of the invention
It is an object of the invention to provide a kind of impulsive force can born and crash through glass, effectively protect firing-fighting medium, improve
The UAV system fire extinguisher bomb of extinguishing effect.
In order to achieve the above object, the technical scheme is that a kind of UAV system fire extinguisher bomb, including taper bullet,
Electronic compartment, body, rear end cap, inner cone bar, to bore bar, stay tube, igniter, electromotor, saucisson and anti-light interference afterwards infrared
Sensor, one end of described taper bullet and inner cone bar is fixing to be connected, and electronic compartment is fixed with one end of body and is connected, rear end cap and
The other end of body is fixing to be connected, and a stay tube is positioned at body, and the other end of inner cone bar is fixing with stay tube one end to be connected, and bores afterwards
Bar is fixing with a stay tube other end and rear end cap to be connected, and described electromotor is fixing with rear end cap to be connected, and is provided with in described stay tube
Saucisson, is provided with gunpowder in saucisson, prop up and be provided with firing-fighting medium between stay tube and body, and igniter is positioned at electronic compartment, and
The ignition fuse of igniter stretches in saucisson, and anti-light interference infrared sensor electrically connects with the wiring board of igniter.
Preferably, described stay tube is Raphel pipe, supports and is uniformly distributed several bellmouth orifices on tube wall.
Preferably, described igniter also includes that battery, battery lead, switch and wiring board, described battery pass through battery
Lead-in wire is connected with wiring board, and battery lead is provided with switch.
Preferably, described battery is annular anti-explosion battery, and be sleeved on inner cone bar.
Preferably, the other end of described inner cone bar is provided with installation projection, installs projection and stretches into pore one end of a stay tube, and
Fixing connection.
Preferably, described rear end cap is provided with mounting flange, and mounting flange is fixing with electromotor to be connected.
Preferably, at least two anti-light interference infrared sensor, the infrared biography of anti-light interference it are also equipped with in described electronic compartment
Sensor electrically connects with the wiring board of igniter.
Preferably, also include that unmanned plane, launching tube and sighting device, described launching tube and sighting device are fixedly connected on nothing
Man-machine bottom, body is positioned at launching tube, and is aimed at by sighting device.
After using said structure, the present invention is additionally arranged the supporting construction to taper bullet on the basis of original fire extinguisher bomb,
Taper bullet is supported by inner cone bar, rear cone bar and a stay tube, and a stay tube is arranged between forward and backward cone bar, and a stay tube not only holds
Load equilibrium is expanded gas explosion stream, is ensured the function of the uniform spreading of firing-fighting medium, and the part bearing taper bullet breaks first extruding force,
Protection firing-fighting medium, enhances brokenly first effect.Firing-fighting medium it is provided with between stay tube and body, when the present invention works, cone
Shape bullet crashes through glass curtain wall and enters indoor flame range, anti-light interference infrared sensor perception flame, starts fire extinguisher bomb immediately and implements
Fire extinguishing.The thrust of electromotor by rear end cap, bore bar afterwards, stay tube, inner cone bar are delivered to taper bullet, when Conical Projectile butt is hit
The extruding force that the resistance being subject to during glass curtain wall and the thrust of electromotor are formed acts on taper bullet, does not form body
Extruding, it is ensured that the safety of body, is then carried out fire extinguishing.
Accompanying drawing explanation
Fig. 1 is the full sectional view of the present invention；
Fig. 2 is the explosive view of Fig. 1；
Fig. 3 is the schematic diagram that Fig. 1 is mounted on unmanned plane.
Detailed description of the invention
The present invention is further detailed explanation for the embodiment be given below in conjunction with accompanying drawing.
Seeing shown in Fig. 1,2,3, a kind of UAV system fire extinguisher bomb, including taper bullet 1, electronic compartment 2, body 3, rear end cap
4, inner cone bar 5, rear cone bar 6, a stay tube 7, igniter 8, electromotor 9, saucisson 20 and anti-light interference infrared sensor 30, institute
Stating that one end of taper bullet 1 and inner cone bar 5 is fixing to be connected, electronic compartment 2 is fixed with one end of body 3 and is connected, rear end cap 4 and body
The other end of 3 is fixing to be connected, and a stay tube 7 is positioned at body 3, and the other end of inner cone bar 5 is fixing with stay tube 7 one end to be connected, after
Cone bar 6 is fixed be connected with stay tube 7 other end and rear end cap 4, and described electromotor 9 is fixing with rear end cap 4 to be connected, described stay tube
It is provided with saucisson 20 in 7, in saucisson 20, is provided with gunpowder, prop up and between stay tube 7 and body 3, be provided with firing-fighting medium 10, igniter 8
Be positioned at electronic compartment 2, and the ignition fuse 81 of igniter 8 stretch in saucisson 20, and anti-light interference infrared sensor 30 with
The wiring board 85 of igniter 8 electrically connects.
See Fig. 1, shown in 2, described stay tube 7 is Raphel pipe, and stay tube 7 tube wall is uniformly distributed several bellmouth orifices
71.Raphael's pipe not only undertakes equilibrium and expands gas explosion stream, ensures the function of the uniform spreading of firing-fighting medium, and can bear Conical Projectile
The 1 broken first extruding force of a part.
Shown in Figure 2, described igniter 8 also includes battery 82, battery lead 83, switch 84 and wiring board 85, institute
State battery 82 to be connected with wiring board 85 by battery lead 83, battery lead 83 is provided with switch 84.Described battery 82 is ring
Shape anti-explosion battery, and be sleeved on inner cone bar 5.Annular made by battery 82, adapts to installation environment in electronic compartment 2.Point given by battery 82
Fire device 8 and anti-light interference infrared sensor 30 provide power supply, control ability and sensitivity higher.
See Fig. 1, shown in 2, in order to play better seal effect, improve installation reliability.Another of described inner cone bar 5
End is provided with installation projection 51, installs protruding 51 pore one end stretching into a stay tube 7, and fixing connection.
See Fig. 1, shown in 2, in order to make electromotor 9 install fixation, electromotor 9 gives power source of the present invention, described
Rear end cap 4 is provided with mounting flange 41, and mounting flange 41 is fixing with electromotor 9 to be connected.
See Fig. 1, shown in 2, in described electronic compartment 2, be also equipped with three anti-light interference infrared sensors 30, anti-light interference
Infrared sensor 30 electrically connects with the wiring board 85 of igniter 8.Three anti-light interference infrared sensors 30 are equal with hexagonal angle degree
Cloth is on electronic compartment 2, if there being a damage, other two serve the same role equally, it is ensured that fire extinguishing is smoothed out.
Shown in Figure 3, also include unmanned plane 40, launching tube 50 and sighting device 60, described launching tube 50 and aiming dress
Putting 60 and be fixedly connected on bottom unmanned plane 40, body 3 is positioned at launching tube 50, and is aimed at by sighting device 60.The present invention's
Fire extinguisher bomb is mounted on unmanned plane 40, and unmanned plane 40 is many rotor wing unmanned aerial vehicles, and launching tube 50 and control system thereof are arranged on nothing
On man-machine 40；Fire extinguisher bomb is contained in launching tube 50, fixes with spring steady pin；Junction point ignition source.Unmanned plane cost is relatively
Low, no one was injured risk, survival ability is strong, mobility good, advantage easy to use etc..
When the present invention uses, being fixed on by fire extinguisher bomb in the launching tube 50 of unmanned plane 40, then unmanned plane takes off, and flies to fire
, before hovering over the window of the building that catch fire；Aimed at by sighting device 60；Releasing faulty action preventing switchs, and igniting is launched, fire extinguisher bomb
Broken window enters flame range.During broken window, the resistance being subject to when taper bullet 1 clashes into glass curtain wall and the thrust of electromotor 9 are formed
Extruding force acts on taper bullet 1, body 3 is not formed extruding, it is ensured that the safety of body 3, protects firing-fighting medium 10,
Anti-light interference infrared sensor 30 contacts flame, and ignition fuse 81 ignites the gunpowder in saucisson 20, produces the gas of some strength
Stream, forms pressure, is forced leave by the air in flame range, and firing-fighting medium 10 covers on comburant with air-flow simultaneously so that it is with air
Isolation, implements fire extinguishing.Current all kinds of extinguishing chemical kind is a lot, and the fire extinguisher bomb of the present invention uses solid, powdery extinguishing chemical.When
So in confined space, it is possible to taking gas extinguishing agent, effect is more preferable.
Above-described is only the preferred embodiment of the present invention, it is noted that for those of ordinary skill in the art
For, without departing from the concept of the premise of the invention, it is also possible to make some deformation and improvement, these broadly fall into the present invention
Protection domain.
Claims (8)
1. a UAV system fire extinguisher bomb, it is characterised in that: include taper bullet (1), electronic compartment (2), body (3), rear end cap
(4), inner cone bar (5), bore bar (6), stay tube (7), igniter (8), electromotor (9), saucisson (20) and anti-light interference afterwards
Infrared sensor (30), described taper bullet (1) is fixing with one end of inner cone bar (5) to be connected, electronic compartment (2) and body (3)
One end is fixing to be connected, and rear end cap (4) is fixing with the other end of body (3) to be connected, and a stay tube (7) is positioned at body (3), inner cone bar
(5) the other end is fixing with stay tube (7) one end to be connected, and bores bar (6) afterwards and fixes with stay tube (7) other end and rear end cap (4)
Connecting, described electromotor (9) is fixing with rear end cap (4) to be connected, and is provided with saucisson (20), saucisson in described stay tube (7)
(20) being provided with gunpowder in, prop up and be provided with firing-fighting medium (10) between stay tube (7) and body (3), igniter (8) is positioned at electronic compartment
(2) in, and in the ignition fuse (81) of igniter (8) stretches into saucisson (20), and anti-light interference infrared sensor (30) with
Wiring board (85) electrical connection of igniter (8).
UAV system fire extinguisher bomb the most according to claim 1, it is characterised in that: described stay tube (7) is Raphel pipe,
Several bellmouth orifices (71) it are uniformly distributed on stay tube (7) tube wall.
UAV system fire extinguisher bomb the most according to claim 1, it is characterised in that: described igniter (8) also includes battery
(82), battery lead (83), switch (84) and wiring board (85), described battery (82) is by battery lead (83) and wiring board
(85) connect, battery lead (83) is provided with switch (84).
UAV system fire extinguisher bomb the most according to claim 3, it is characterised in that: described battery (82) is annular anti-explosion electric
Pond, and be sleeved on inner cone bar (5).
UAV system fire extinguisher bomb the most according to claim 1, it is characterised in that: the other end of described inner cone bar (5) is provided with
Projection (51) is installed, protruding (51) is installed and stretches into pore one end of a stay tube (7), and fixing connection.
UAV system fire extinguisher bomb the most according to claim 1, it is characterised in that: described rear end cap (4) is provided with Method for Installation
Blue (41), mounting flange (41) is fixing with electromotor (9) to be connected.
UAV system fire extinguisher bomb the most according to claim 6, it is characterised in that: be also equipped with in described electronic compartment (2) to
Few two anti-light interference infrared sensors (30), anti-light interference infrared sensor (30) is arranged in electronic compartment (2).
UAV system fire extinguisher bomb the most according to claim 1, it is characterised in that: also include unmanned plane (40), launching tube
(50) and sighting device (60), described launching tube (50) is fixedly connected on unmanned plane (40) end by buckle and latchplate (51)
Portion, sighting device (60) and launching tube (50) are arranged on unmanned plane (40) bottom side by side, and body (3) is positioned at launching tube (50),
And aimed at by sighting device (60).
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610892816.9A CN106267637B (en) | 2016-10-12 | 2016-10-12 | Unmanned aerial vehicle carries fire extinguishing bomb |
| CN201621119108.3U CN206228812U (en) | 2016-10-12 | 2016-10-12 | A kind of UAV system fire extinguisher bomb |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610892816.9A CN106267637B (en) | 2016-10-12 | 2016-10-12 | Unmanned aerial vehicle carries fire extinguishing bomb |
| CN201621119108.3U CN206228812U (en) | 2016-10-12 | 2016-10-12 | A kind of UAV system fire extinguisher bomb |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106267637A true CN106267637A (en) | 2017-01-04 |
| CN106267637B CN106267637B (en) | 2022-08-19 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621119108.3U Active CN206228812U (en) | 2016-10-12 | 2016-10-12 | A kind of UAV system fire extinguisher bomb |
| CN201610892816.9A Active CN106267637B (en) | 2016-10-12 | 2016-10-12 | Unmanned aerial vehicle carries fire extinguishing bomb |
Family Applications Before (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621119108.3U Active CN206228812U (en) | 2016-10-12 | 2016-10-12 | A kind of UAV system fire extinguisher bomb |
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| Country | Link |
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Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| CN107158602A (en) * | 2017-04-27 | 2017-09-15 | 陶霖密 | A kind of emission type disaster relief and unmanned plane and fire-extinguishing |
| CN107264802A (en) * | 2017-06-27 | 2017-10-20 | 北京电子工程总体研究所 | A kind of unmanned plane fire extinguisher bomb glass penetration test system and test method |
| CN107388891A (en) * | 2017-04-12 | 2017-11-24 | 江苏溧航航空科技有限公司 | A kind of UAV system fire extinguishing bullet launching device |
| CN107670201A (en) * | 2017-08-31 | 2018-02-09 | 上海机电工程研究所 | UAV system type fire extinguishing system |
| CN108744354A (en) * | 2018-04-26 | 2018-11-06 | 西北工业大学 | A kind of airborne fire extinguisher bomb |
| CN108771803A (en) * | 2018-08-10 | 2018-11-09 | 中国人民解放军火箭军工程大学 | Control system and fire extinguishing system for the fire extinguishing of skyscraper rotor wing unmanned aerial vehicle |
| CN109316689A (en) * | 2018-09-28 | 2019-02-12 | 芜湖博高光电科技股份有限公司 | A kind of anti-re-ignition fire extinguisher bomb of non-toggle combined fuze |
| CN109945748A (en) * | 2019-04-12 | 2019-06-28 | 江西剑安消防科技有限责任公司 | A kind of unmanned plane wisdom fire extinguishing bomb special |
| US20230308042A1 (en) * | 2022-01-27 | 2023-09-28 | Ameristar Solar, LLC | SOLAR eVTOL DRONE TOWER |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN206228812U (en) * | 2016-10-12 | 2017-06-09 | 江苏溧航航空科技有限公司 | A kind of UAV system fire extinguisher bomb |
| CN112325706B (en) * | 2020-11-04 | 2024-06-18 | 江苏溧航航空科技有限公司 | Unmanned vehicles-based bundling fire extinguishing bomb device for forest fire extinguishment |
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Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107388891A (en) * | 2017-04-12 | 2017-11-24 | 江苏溧航航空科技有限公司 | A kind of UAV system fire extinguishing bullet launching device |
| CN107388891B (en) * | 2017-04-12 | 2023-07-18 | 江苏溧航航空科技有限公司 | Unmanned aerial vehicle carries fire extinguishing bomb emitter |
| CN107158602A (en) * | 2017-04-27 | 2017-09-15 | 陶霖密 | A kind of emission type disaster relief and unmanned plane and fire-extinguishing |
| 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 |
| CN107264802A (en) * | 2017-06-27 | 2017-10-20 | 北京电子工程总体研究所 | A kind of unmanned plane fire extinguisher bomb glass penetration test system and test method |
| CN107670201A (en) * | 2017-08-31 | 2018-02-09 | 上海机电工程研究所 | UAV system type fire extinguishing system |
| CN108744354B (en) * | 2018-04-26 | 2023-06-23 | 西北工业大学 | Machine carries fire extinguishing bomb |
| CN108744354A (en) * | 2018-04-26 | 2018-11-06 | 西北工业大学 | A kind of airborne fire extinguisher bomb |
| CN108771803A (en) * | 2018-08-10 | 2018-11-09 | 中国人民解放军火箭军工程大学 | Control system and fire extinguishing system for the fire extinguishing of skyscraper rotor wing unmanned aerial vehicle |
| CN108771803B (en) * | 2018-08-10 | 2023-09-15 | 李�杰 | Control system for high-rise building rotor unmanned aerial vehicle fire extinguishment and fire extinguishing system |
| CN109316689A (en) * | 2018-09-28 | 2019-02-12 | 芜湖博高光电科技股份有限公司 | A kind of anti-re-ignition fire extinguisher bomb of non-toggle combined fuze |
| CN109945748B (en) * | 2019-04-12 | 2022-02-15 | 江西剑安消防科技有限责任公司 | Method for assembling intelligent special fire extinguishing bomb for unmanned aerial vehicle |
| CN109945748A (en) * | 2019-04-12 | 2019-06-28 | 江西剑安消防科技有限责任公司 | A kind of unmanned plane wisdom fire extinguishing bomb special |
| US20230308042A1 (en) * | 2022-01-27 | 2023-09-28 | Ameristar Solar, LLC | SOLAR eVTOL DRONE TOWER |
Also Published As
| Publication number | Publication date |
|---|---|
| CN206228812U (en) | 2017-06-09 |
| CN106267637B (en) | 2022-08-19 |
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Address after: 213000 No. 8-5 Huashan Road, Xinbei District, Changzhou City, Jiangsu Province Applicant after: JIANGSU LIHANG AVIATION TECHNOLOGY CO.,LTD. Address before: 213000 Dongcheng Mingju Building 801, Tianning District, Changzhou City, Jiangsu Province Applicant before: JIANGSU LIHANG AVIATION TECHNOLOGY CO.,LTD. |
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