CN201668907U - Long-range multi-barrel fire-extinguishing rocket and launching apparatus thereof - Google Patents
Long-range multi-barrel fire-extinguishing rocket and launching apparatus thereof Download PDFInfo
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- CN201668907U CN201668907U CN2010201852190U CN201020185219U CN201668907U CN 201668907 U CN201668907 U CN 201668907U CN 2010201852190 U CN2010201852190 U CN 2010201852190U CN 201020185219 U CN201020185219 U CN 201020185219U CN 201668907 U CN201668907 U CN 201668907U
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- extinguishing
- rocket projectile
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Abstract
The utility model relates to a long-range multi-barrel fire-extinguishing rocket and a launching apparatus thereof. Launching barrels (2) are horizontally and vertically arranged in a launcher (1), which is a box; a hydraulic electric lifter (5) is arranged between the launcher (1) and a gimbaled base (3); a launching ignition system (6), a positioning terminal system (7), a charging controller (8) and a storage battery (9) are arranged on the gimbaled base (3); the body structure of the rocket (4) consists of a sensor (10), an infrared sensor (11), an igniter (12), compressed fire-extinguishing dry powder (13), a heat-insulating board (14), a combustion chamber (15), an ignition door (16), a fairing (17) and a rocket shell (18), wherein the rocket shell (18) is made of a paper tube or plastic, and the heat-insulating board (14) is made of high temperature-resistant fibers and ceramic heat-insulating material. The utility model has the advantages of reliable control, quick response, extremely high fire-extinguishing efficiency and accurate fire scene strike, and cannot be affected by the distance of a fire scene, and in particular, the utility model has a special fire-extinguishing effect on a large-area strong fire scene, and can extinguish an initial fire within the shortest time.
Description
Technical field: the utility model belongs to fire-fighting equipment, forest extinguishing device technique field.
Background technology: at present, for forest fire, the normal in the world extinguishing method that adopts is that personnel put out the fire, carry powerful hair-dryer, blow out burning things which may cause a fire disaster, perhaps excavate the isolation strip, make the intensity of a fire in the isolation strip by isolation and voluntarily breath go out, perhaps adopt helicopter to carry water tank and spread water and put out burning things which may cause a fire disaster.These modes all exist defective and deficiency separately.The employing personnel put out a fire with powerful hair-dryer, generally only limit to little fire, block fire or fragmentary fire, if the intensity of a fire is big, personnel at all can't be near the scene of a fire, let alone handles the problem of hair-dryer fire extinguishing; Excavation isolation strip and wall with flues are a kind of comparatively effective methods at big fire, but digging process is time-consuming, can not tackle the urgent of the intensity of a fire in the time of many at all and spread, and excavate the isolation strip again in place far away, then lost a large amount of forests and vegetation, but also will lose a large amount of forests and vegetation with the broad isolation strip of the reply intensity of a fire itself.Forest fire is normally burnt in mountain valley far away, distance cities and towns, physical features is strategically located and difficult of access, have inconvenient traffic, the fire fighting personnel short time will be arrived in very difficulty of the scene of a fire, adopt helicopter to hang the water tank fire-fighting mode, be only applicable to just on firely, fire point is concentrated, burning hot little situation, helicopter is fetched water also very inconvenient back and forth, a water intaking will fly tens minutes sometimes, even dozens of minutes just can get water to remote water field, and the big fire of just having been put out by water by water, very fast revivable under the effect of fragmentary burning things which may cause a fire disaster and wind-force, roll exceedingly high big fire again, under strong burning hot state, the fire fighting personnel also fully can't be near big fire, countries in the world almost have nothing effective at present, and way is put out it, mostly helplessly wait for it with forest zone burning totally, self breath goes out, and enters the scene of a fire after the burning by the fire extinguishing personnel at last and clears up and drop.
Summary of the invention: the purpose of this utility model, providing a kind of in order to overcome defective that above-mentioned fire-fighting mode exists and weak point does not just need personnel to rush for the scene of a fire rapidly, can be in the shortest time, the remote relatively scene of a fire, at that I guess the strongest big fire, take to locate accurately, fixed point, low latitude blast mode put out a fire the device that big fire can be put out at one stroke in the shortest time.
The purpose of this utility model is achieved by the following technical solution.
The utility model comprises launcher, transmitting tube and gimballed base and fire extinguishing rocket projectile body, it is characterized in that, is arranged in the launcher by the transmitting tube that is no less than is vertically and horizontally arranged, and launcher is a body structure; Center between launcher and gimballed base is provided with a hydraulic electric lift; On gimballed base, also be provided with launch point ignition system, locating terminal system, charge controller and battery; The body structure of rocket projectile is, from the head to afterbody: sensor, infrared survey sense instrument, apparatus to cause bursting, compression fire-fighting powder, thermal insulation board, combustion chamber, lighting door, preceding bullet lid and body; Wherein the body material is paper web or plastics, and thermal insulation board is refractory fibrous material and ceramic insulating material; The main devices of infrared induction instrument is a pyroelectric sensor, and pyroelectric sensor is by amplifier, wave filter, and level comparator, drive circuit, relay and voltage-stabilized power supply constitute.
The utility model also is provided with solar energy silicon wafer plate in the top plan of launcher; The utility model also gimballed base is provided with the bracing frame of being with vibration absorber; The whole gimballed base of the present invention be arranged on the automobile chassis or the wheel load chassis of trailer on, when adopting the wheel load chassis of trailer, be provided with the traction hook at the trailer front end.
The beneficial effects of the utility model are that control is reliable, and is rapidly emergent, not limit by scene of a fire far and near distance, fire extinguishing effectiveness is high, and the strike scene of a fire is accurate, especially the fire extinguishing of the surging scene of a fire has special-effect to large tracts of land, and has more the remarkable advantage that the intensity of a fire that can will just fire was put out in the shortest time.
Further set forth content of the present utility model below in conjunction with drawings and Examples.
Description of drawings: Fig. 1 is provided with schematic diagram for the utility model structure;
Fig. 2 is fire extinguishing rocket projectile structural representation.
The specific embodiment:
The utility model comprises launcher 1, transmitting tube 2 and gimballed base 3 and rocket projectile 4 bodies, it is characterized in that, by transmitting tube 2 vertically and horizontally arranged being arranged in the launcher 1 that are no less than, launcher 1 is a body structure; Center between launcher 1 and gimballed base 3 is provided with a hydraulic electric lift 5; On gimballed base 3, also be provided with launch point ignition system 6, locating terminal system 7, charge controller 8 and battery 9; The body structure of rocket projectile 4 is, from the head to afterbody: sensor 10, infrared survey sense instrument 11, apparatus to cause bursting 12, compression fire-fighting powder 13, thermal insulation board 14, combustion chamber 15, lighting door 16, preceding bullet lid 17 and body 18; Wherein body 18 materials are paper web or plastics, and thermal insulation board is a refractory fibrous material; The main devices of infrared induction instrument 11 is pyroelectric sensors 10, and pyroelectric sensor 10 is by amplifier, wave filter, and level comparator, drive circuit, relay and voltage-stabilized power supply constitute.
The utility model also is provided with solar energy silicon wafer plate 19 in the top plan of emission support body 1; The present invention also gimballed base 3 is provided with the bracing frame 20 of being with vibration absorber; The whole gimballed base 3 of the present invention be arranged on the automobile chassis or wheel load chassis of trailer 21 on, when adopting the wheel load chassis of trailer, be provided with traction hook 22 at the trailer front end.
Owing to adopt the mode of rocket launching, emission by long-range box fire extinguishing launcher 1, many fire extinguishing rocket projectiles 2 can be transmitted into the scene of a fire in moment puts out a fire, and be arranged on sensor 10 on the rocket projectile point that goes out, the area that is measured by infrared survey sense instrument 11 in the locating terminal system 7 transmission bodies that are arranged on the launcher gimballed base 3, the orientation, signal apart from ground location, and being database itself by locating terminal system 7, the accurate position in the scene of a fire can provide, in case the fire extinguishing rocket projectile is arrived in the sky, the scene of a fire by plane, and the accurate distance of setting apart from ground, the position of two meters or five meters overhead for example, trigger apparatus to cause bursting 12 by transducing signal, body 18 explosions with body paper web or plastic material, compressed fire-fighting powder moment is expanded rapidly, and it is isolated that every resilience energy will have an area of in 100~500 square metres of scopes oxygen, and dry powder also plays the effect of putting out to flame simultaneously, product is a lot of in the present city of fire-fighting powder agent, can select according to scene of a fire situation.The sensor of rocket projectile and infrared survey sense instrument remove if will put out a fire, and can become fixed point, concentrate the system and device of fire extinguishing emission.The utility model adopts the mass-sending of box-type multi-tube launcher, in a short period of time large-area forest fire is put out.Adopt at present the locating terminal system, for example GPS locating terminal system and infrared survey sense instrument and sensor, the technology of measuring accurate target is maturation quite.
The main devices that infrared induction is driven instrument is a pyroelectric sensor, amplifier, and wave filter, level comparator, drive circuit, relay and voltage-stabilized power supply constitute pyroelectric sensor.Pyroelectric infrared sensor, we know that any object that is higher than absolute zero all can discharge infrared spectrum, the object of different temperatures, the wavelength of the infrared energy of its release is different, so infrared wavelength is relevant with the height of temperature.You are reflected on the PIR by luxuriant and rich with fragrance mud, and optical filter gathers on the infrared induction source after strengthening.The pyroelectricity element is adopted in the infrared induction source usually, and this element will lose charge balance when infrared radiation temperature changes receiving, and outwards discharges electric charge, and subsequent conditioning circuit is handled the back after testing just can the trigger switch action.So long as the object that temperature arranged all can to around infrared radiation, when hot object enters the infrared induction scope, probe is collected extraneous infra-red radiation by gathering the variation that detects the hot object infrared spectrum on the infrared induction source, infrared inductor is exactly to receive the infrared ray that those objects send by sensor, amplifying, connect load automatically and ignite fire extinguisher bomb through oversampling circuit.
The definition of " long-range " is at distance, and is described in the utility model long-range, generally can be in 5~100 kilometers distance, and the length of distance, the main fire extinguishing rocket projectile combustion chamber size that relies on is how much determining of fuel.The emission support body adopts the box-type multi-tube structure, is in order to launch many fire extinguishing rocket projectiles simultaneously after determining target, at large stretch of scene of a fire of advantage burning, concentrates simultaneously it is extinguished, and prevents peripheral intensity of a fire resume combustion.The box-type multi-tube structure, 1~6 row's transmitting tube is arranged usually, every row has 4~10 pipe transmitting tubes, the overall emission frame is by being positioned at the emission angle that the passive hydraulic electric lift in center, casing below supported and regulated simultaneously the emission support body, the hydraulic electric lift is arranged on the gimballed base, this gimballed base is provided with the bracing frame of band vibration absorber, be used for when the emission body, be supported on ground and play the effect of vibrationproof vibration damping, whole gimballed base promptly can be a structure support body, also can integral body be set to be installed on the automobile chassis, or be a wheel load trailer, by vehicle traction.Like this, the utility model device can be travelled at short notice to arrive at and anyly have the place of highway to install and use rapidly.The electric energy of whole launcher is provided by the batteries that is arranged on the gimballed base.In order to ensure the electricity consumption of the utility model in remote districts and mountain forest area, the present invention all is set to device of solar generating with silicon crystal slate with plane, the case of box emission support body top, utilize charge controller constantly to be battery charging, it is standby to make it guarantee to be full of electricity constantly; Certainly, under continuous many days cloudy situations, also can adopt commercial power charged.Fire extinguishing rocket airframe head is exposed at outside the emission casing, the bottom priming door is lighted a fire by the launch point ignition control system, the indoor propellant of lighting door pilot combustion of body, body just flies away from casing at a high speed along the helix moment in the transmitting tube, the target that directive is set, certainly, if case material of the present utility model and extinguishing chemical are replaced with military material, then the utility model can be directly used in military purposes.
Claims (4)
1. remote multi-tube fire extinguishing rocket projectile and emitter thereof, comprise launcher (1), transmitting tube (2), gimballed base (3) and rocket projectile (4) body, it is characterized in that be arranged in the emission support body (1) by the transmitting tube (2) that is no less than is vertically and horizontally arranged, launcher (1) is a body structure; Center between launcher (1) and gimballed base (3) is provided with a hydraulic electric lift (5); On gimballed base (3), also be provided with launch point ignition system (6), locating terminal system (7), charge controller (8) and battery (9); The body structure of rocket projectile (4) is, from the head to afterbody: sensor (10), infrared survey sense instrument (11), apparatus to cause bursting (12), compression fire-fighting powder (13), thermal insulation board (14), combustion chamber (15), lighting door (16), preceding bullet lid (17) and body (18); Wherein body (18) material is paper web or plastics, and thermal insulation board (14) is refractory fibrous material and ceramic insulating material; The main devices of infrared induction instrument (11) is pyroelectric sensor (10), and pyroelectric sensor (10) is by amplifier, wave filter, and level comparator, drive circuit, relay and voltage-stabilized power supply constitute.
2. remote multi-tube fire extinguishing rocket projectile according to claim 1 and emitter thereof is characterized in that, are provided with solar energy silicon wafer plate (19) in the top plan of launching support body (1).
3. remote multi-tube fire extinguishing rocket projectile according to claim 1 and emitter thereof is characterized in that gimballed base (3) is provided with the bracing frame (20) of band vibration absorber.
4. remote multi-tube fire extinguishing rocket projectile according to claim 1 and emitter thereof, it is characterized in that, whole gimballed base (3) be arranged on the automobile chassis or wheel load chassis of trailer (21) on, when adopting the wheel load chassis of trailer, be provided with traction hook (22) at the trailer front end.
Priority Applications (1)
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CN2010201852190U CN201668907U (en) | 2010-05-11 | 2010-05-11 | Long-range multi-barrel fire-extinguishing rocket and launching apparatus thereof |
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CN2010201852190U CN201668907U (en) | 2010-05-11 | 2010-05-11 | Long-range multi-barrel fire-extinguishing rocket and launching apparatus thereof |
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Cited By (8)
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CN102935274A (en) * | 2012-11-16 | 2013-02-20 | 青岛科而泰环境控制技术有限公司 | Liquid projection bomb, projecting device and delivery method thereof |
CN103925839A (en) * | 2014-04-29 | 2014-07-16 | 成都陵川特种工业有限责任公司 | Fire-extinguishing bullet launcher |
CN104645533A (en) * | 2013-11-20 | 2015-05-27 | 安长海 | Intelligent mechanical remote fire-extinguishing device with fixed-point launching |
CN104916208A (en) * | 2015-06-09 | 2015-09-16 | 贺中秋 | Model rocket launching vehicle |
CN106019989A (en) * | 2016-05-10 | 2016-10-12 | 中国人民解放军海军工程大学 | Security control method for multi-tube emission system |
CN106075785A (en) * | 2016-06-28 | 2016-11-09 | 成都启源电子信息技术有限公司 | Intelligent fire fighting discharger |
CN106267637A (en) * | 2016-10-12 | 2017-01-04 | 江苏溧航航空科技有限公司 | UAV system fire extinguisher bomb |
CN109813180A (en) * | 2018-12-03 | 2019-05-28 | 南京航空航天大学 | A kind of air bubble localizing emission control system and control method based on rotating vane |
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2010
- 2010-05-11 CN CN2010201852190U patent/CN201668907U/en not_active Expired - Fee Related
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
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CN102935274B (en) * | 2012-11-16 | 2015-12-30 | 青岛科而泰环境控制技术有限公司 | A kind of liquid projection bullet and grenade instrumentation thereof and delivering method |
US9795814B2 (en) | 2012-11-16 | 2017-10-24 | Qingdao Create Environment Control Technology Co., Ltd. | Liquid projection bomb, projecting device and delivery method therefor |
CN102935274A (en) * | 2012-11-16 | 2013-02-20 | 青岛科而泰环境控制技术有限公司 | Liquid projection bomb, projecting device and delivery method thereof |
CN104645533A (en) * | 2013-11-20 | 2015-05-27 | 安长海 | Intelligent mechanical remote fire-extinguishing device with fixed-point launching |
CN103925839B (en) * | 2014-04-29 | 2015-08-19 | 成都陵川特种工业有限责任公司 | A kind of fire-extinguishing shell launcher |
CN103925839A (en) * | 2014-04-29 | 2014-07-16 | 成都陵川特种工业有限责任公司 | Fire-extinguishing bullet launcher |
CN104916208A (en) * | 2015-06-09 | 2015-09-16 | 贺中秋 | Model rocket launching vehicle |
CN106019989A (en) * | 2016-05-10 | 2016-10-12 | 中国人民解放军海军工程大学 | Security control method for multi-tube emission system |
CN106075785A (en) * | 2016-06-28 | 2016-11-09 | 成都启源电子信息技术有限公司 | Intelligent fire fighting discharger |
CN106267637A (en) * | 2016-10-12 | 2017-01-04 | 江苏溧航航空科技有限公司 | UAV system fire extinguisher bomb |
CN106267637B (en) * | 2016-10-12 | 2022-08-19 | 江苏溧航航空科技有限公司 | Unmanned aerial vehicle carries fire extinguishing bomb |
CN109813180A (en) * | 2018-12-03 | 2019-05-28 | 南京航空航天大学 | A kind of air bubble localizing emission control system and control method based on rotating vane |
CN109813180B (en) * | 2018-12-03 | 2021-03-30 | 南京航空航天大学 | Air cannon positioning and launching control system and control method based on rotating blades |
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Legal Events
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C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20101215 Termination date: 20150511 |
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EXPY | Termination of patent right or utility model |