CN111589016A - High-altitude aviation fire extinguishing and disaster relief system - Google Patents
High-altitude aviation fire extinguishing and disaster relief system Download PDFInfo
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- CN111589016A CN111589016A CN202010356034.XA CN202010356034A CN111589016A CN 111589016 A CN111589016 A CN 111589016A CN 202010356034 A CN202010356034 A CN 202010356034A CN 111589016 A CN111589016 A CN 111589016A
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- 239000000725 suspension Substances 0.000 claims description 17
- 230000005484 gravity Effects 0.000 claims description 13
- 239000003795 chemical substances by application Substances 0.000 description 17
- 238000000034 method Methods 0.000 description 6
- 241000282414 Homo sapiens Species 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 239000000463 material Substances 0.000 description 3
- 239000003721 gunpowder Substances 0.000 description 2
- 230000001629 suppression Effects 0.000 description 2
- 238000009412 basement excavation Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
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- 238000005516 engineering process Methods 0.000 description 1
- 239000011796 hollow space material Substances 0.000 description 1
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- 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
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- 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
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- 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
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- A—HUMAN NECESSITIES
- A62—LIFE-SAVING; FIRE-FIGHTING
- A62C—FIRE-FIGHTING
- A62C31/00—Delivery of fire-extinguishing material
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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
- F42B12/50—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 by dispersion
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- Forests & Forestry (AREA)
- General Engineering & Computer Science (AREA)
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- Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
Abstract
The invention relates to a high-altitude aviation fire extinguishing and disaster relieving system, which comprises an aerial carrying platform, and a throwing fire extinguishing system and a guiding fire extinguishing system which are arranged on the aerial carrying platform; the throwing fire extinguishing system comprises an annular throwing frame and a plurality of free falling body fire fighting bombs arranged at the lower end of the annular throwing frame, and the guidance fire extinguishing system comprises a launching cabin and a plurality of aviation guidance fire fighting bombs arranged in the launching cabin. The invention takes a manned low-speed low-altitude aircraft or an unmanned aerial robot as an aerial carrying platform to carry a throwing fire extinguishing system and a guiding fire extinguishing system, thereby respectively realizing the fire extinguishing and disaster relief operation on open-air fire or high-rise building fire.
Description
Technical Field
The invention relates to the technical field of fire extinguishing and disaster relief appliances, in particular to a high-altitude aviation fire extinguishing and disaster relief system.
Background
Along with social progress and technical development, the damage and influence of human survival and activities on the natural environment are increased continuously, the change of human living conditions causes various fires to occur frequently, fire fighting, fire extinguishing and disaster relief are serious major problems for human beings, and no scientific and efficient effective method exists at present for continuously occurring forest fires and high-rise building fires. Once a forest fire occurs, the method has the characteristics of rapid fire development, high fire-fighting difficulty, long disaster time, serious resource loss and the like, the conventional fire-fighting method still adopts the conventional methods such as ground manual fire-fighting, mechanical fire-fighting, isolation zone excavation and the like, the fire-fighting helicopter is used for fire-fighting in air fire-fighting, and the conventional helicopter is used for fire-fighting, so that the following problems exist, such as no wide water surface near a fire source, difficult helicopter fire-fighting, low remote water taking efficiency and high cost, the too high fire-fighting efficiency of helicopter flight is poor due to the unsteady airflow change of a fire airspace above a fire area, and the life of a flying helicopter driver is threatened. The urban high-rise building fire extinguishing and fire fighting difficulty is higher, the existing urban fire fighting truck cannot achieve the purpose of fire extinguishing and fire fighting of the high-rise building, the existing fire extinguishing and fire fighting scheme cannot solve the problem of urban traffic congestion, once a traffic channel and a fire fighting channel are congested, the existing fire extinguishing and fire fighting technologies and methods cannot achieve the purpose of fire extinguishing and fire fighting.
Disclosure of Invention
The invention aims to provide a high-altitude aviation fire extinguishing and disaster relieving system, which solves the technical problems of high fire extinguishing work difficulty and low fire extinguishing efficiency in the hollow space in the prior art.
In order to achieve the purpose, the technical scheme of the invention is as follows:
a high-altitude aviation fire extinguishing and relief system comprises an aerial carrying platform, a throwing fire extinguishing system and a guidance fire extinguishing system, wherein the throwing fire extinguishing system and the guidance fire extinguishing system are arranged on the aerial carrying platform;
the throwing fire extinguishing system comprises an annular throwing frame and a plurality of free-falling body fire extinguishing bombs arranged at the lower end of the annular throwing frame, the annular throwing frame is fixed at the central position below an aerial carrying platform, the annular throwing frame comprises a suspension buckle, the upper end of the suspension buckle is connected below the aerial carrying platform, the lower end of the suspension buckle is connected with a plurality of connecting frame bodies, the lower ends of the plurality of connecting frame bodies are connected with a suspension ring frame, the suspension ring frame is connected with a plurality of fire extinguishing bomb lifting ropes at equal intervals, each fire extinguishing bomb lifting rope is provided with an electronic lock catch, and the plurality of free-falling body fire extinguishing bombs are connected with the respective fire extinguishing bomb lifting ropes through the electronic lock catches;
the guidance fire extinguishing system comprises a launching cabin and a plurality of aviation guidance fire-fighting bombs arranged in the launching cabin, wherein the launching cabin is of a vertical single-row cabin structure and comprises a plurality of bomb carrying cavities, each bomb carrying cavity is internally provided with the aviation guidance fire-fighting bombs, an electronic lock and an ignition control circuit are arranged in the launching cabin, and the launching cabin is connected below the aerial carrying platform through a universal ring.
Further, the free fall fire control bomb comprises a high-pressure gas cylinder, a gravity impact control valve, a pressure air gathering cabin and an efficient fire-fighting agent bag, wherein the high-pressure gas cylinder is arranged at the tail of the free fall fire control bomb, high-pressure air is stored in the high-pressure gas cylinder, the gravity impact control valve is arranged at the front end of the high-pressure gas cylinder, the high-pressure gas cylinder is communicated with the pressure air gathering cabin through the gravity impact control valve, the pressure air gathering cabin is of a container structure with small bearing force, and the efficient fire-fighting agent bag is wrapped outside the pressure air gathering cabin.
Furthermore, the aviation guidance fire-fighting bomb comprises a thrust part, a guidance rudder wing, a high-pressure gas cylinder, a high-pressure gas control valve, a pressure air gathering cabin, a high-efficiency fire-fighting agent bag and a window breaking warhead; the aviation guidance fire control bomb is characterized in that the guidance rudder wing is arranged at the tail part of the aviation guidance fire control bomb, the thrust part is arranged at the tail end of the aviation guidance fire control bomb, the front end of the thrust part is provided with a high-pressure gas cylinder, high-pressure air is stored in the high-pressure gas cylinder, the front end of the high-pressure gas cylinder is provided with a high-pressure gas control valve, the high-pressure gas cylinder is communicated with a pressure air gathering cabin through the high-pressure gas control valve, the outside of the pressure air gathering cabin is wrapped with an efficient fire-fighting agent bag, and a window breaking.
Further, the aerial embarkation platform comprises an autonomous flight aerial robot or a manned aircraft.
Further, the autonomous flight aerial robot comprises an unmanned helicopter, an unmanned fixed wing airplane and an unmanned remote control airship.
Furthermore, the guide rudder wing is an X-shaped guide wing.
Furthermore, the window breaking warhead is a cone-shaped frame structure warhead and is arranged at the end of the aviation guidance fire-fighting bomb through four rigid rods.
Compared with the prior art, the invention has the following beneficial effects:
the manned low-speed low-altitude aircraft or the unmanned aerial robot is used as an aerial carrying platform to carry a throwing fire extinguishing system and a guiding fire extinguishing system, so that the fire extinguishing and disaster relief operation for outdoor fire or high-rise building fire is realized respectively; the throwing fire extinguishing system throws the free-fall fire bomb loaded with the high-efficiency fire extinguishing agent or other fire fighting materials to a fire area from the upside of the fire area, the free-fall fire bomb is triggered to explode through gravity, and the high-efficiency fire extinguishing agent is thrown to the surrounding fire area, so that the purposes of fire extinguishing and fire relief are achieved; the guidance fire extinguishing system launches the aviation guidance fire bomb to a high-rise building fire area from an aerial window breaking through a launching cabin, and the purpose of quickly and efficiently extinguishing and rescuing is achieved.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings of the embodiments can be obtained according to the drawings without creative efforts.
FIG. 1 is a schematic structural view of a fire suppression throwing system of the present invention;
FIG. 2 is a schematic structural view of a free fall fire-fighting bomb according to the present invention;
FIG. 3 is a schematic structural view of the guided fire suppression system of the present invention;
FIG. 4 is a side view of FIG. 3;
fig. 5 is a schematic structural diagram of the aviation guidance fire bomb provided by the invention.
In the figure, 1-free falling body fire bomb, 2-suspension buckle, 3-connection frame body, 4-suspension ring frame, 5-fire bomb lifting rope, 6-electronic lock catch, 7-launching cabin, 8-aviation guidance fire bomb, 9-high pressure gas cylinder, 10-gravity impact control valve, 11-pressure air gathering cabin, 12-high efficiency fire extinguishing agent bag, 13-thrust part, 14-guidance rudder wing, 15-high pressure gas control valve, 16-window breaking warhead and 17-universal ring.
Detailed Description
To facilitate an understanding of the invention, the invention will now be described more fully with reference to the accompanying drawings. Preferred embodiments of the present invention are shown in the drawings. This invention may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete.
A high-altitude aviation fire extinguishing and relief system comprises an aerial carrying platform, a throwing fire extinguishing system and a guidance fire extinguishing system, wherein the throwing fire extinguishing system and the guidance fire extinguishing system are arranged on the aerial carrying platform;
wherein:
referring to fig. 1, the throwing fire extinguishing system comprises an annular throwing frame and even-numbered free-falling body fire-fighting bombs 1 arranged at the lower end of the annular throwing frame, for example, four-, six-and eight-numbered symmetrical loading, the annular throwing frame is fixed at the central position below an aerial carrying platform, the annular throwing frame comprises suspension buckles 2, the upper ends of the suspension buckles 2 are connected below the aerial carrying platform, the lower ends of the suspension buckles 2 are connected with a plurality of connecting frame bodies 3, the lower ends of the plurality of connecting frame bodies 3 are connected with suspension ring frames 4, the suspension ring frames 4 are connected with a plurality of fire-fighting bomb lifting ropes 5 at equal intervals, each fire-fighting bomb lifting rope 5 is provided with an electronic lock catch 6, and a plurality of free-falling body fire-fighting bombs 1 are connected with the respective fire-fighting bomb;
referring to fig. 2, the free fall fire-fighting bomb 1 comprises a high-pressure gas cylinder 9, a gravity impact control valve 10, a pressure air gathering chamber 11 and an efficient fire-fighting agent bag 12, wherein the high-pressure gas cylinder 9 is arranged at the tail of the free fall fire-fighting bomb 1, high-pressure air is stored in the high-pressure gas cylinder 9, the gravity impact control valve 10 is arranged at the front end of the high-pressure gas cylinder 9, the high-pressure gas cylinder 9 is communicated with the pressure air gathering chamber 11 through the gravity impact control valve 10, the pressure air gathering chamber 11 is of a container structure with small bearing capacity, and the efficient fire-fighting agent bag 12 is wrapped outside the pressure air gathering chamber 11.
Referring to fig. 3 and 4, the guidance fire extinguishing system includes launching cabin 7 and a plurality of pieces of aviation guidance fire control bomb 8 of setting in launching cabin 7, and launching cabin 7 is the single storehouse structure of erectting, including four year bomb cavity, all establishes in every year bomb cavity aviation guidance fire control bomb 8, is equipped with electronic lock and ignition control circuit in the launching cabin, and the launching cabin passes through universal ring 17 and connects in the below of aerial year platform. The launching sequence of the aviation guidance fire-fighting bomb 8 is sequentially launched from bottom to top, the bottom is a missile launching position, when the aviation guidance fire-fighting bomb 8 is launched, the electronic lock of the aviation guidance fire-fighting bomb 8 at the launching position is unlocked, after the aviation guidance fire-fighting bomb 8 is launched, the electronic locks of a plurality of aviation guidance fire-fighting bombs 8 at the upper part of the aviation guidance fire-fighting bomb are unlocked integrally, and the aviation guidance fire-fighting bomb 8 moves downwards and is locked automatically to wait for next launching unlocking.
Referring to fig. 5, the aviation guidance fire-fighting bomb 8 comprises a thrust part 13, a guidance rudder wing 14, a high-pressure gas cylinder 9, a high-pressure gas control valve 15, a pressure air gathering cabin 11, a high-efficiency fire-fighting agent bag 12 and a window breaking warhead 16; the aviation guidance fire-fighting bomb 8 comprises a guidance rudder wing 14, a thrust part 13, a high-pressure gas cylinder 9, a high-pressure air cylinder 9, a high-pressure gas control valve 15, a high-pressure gas cylinder 9, a high-efficiency fire-fighting agent bag 12, a window breaking warhead 16 and four rigid rods, wherein the guidance rudder wing 14 is arranged at the tail part of the aviation guidance fire-fighting bomb 8, the thrust part 13 is arranged at the tail end of the aviation guidance fire-fighting bomb 8, the high-pressure gas cylinder 9 is arranged at the front end of the thrust part 13, high-pressure air is stored in the high-pressure gas cylinder 9, the high-pressure gas control valve 15 is arranged at the front end of the high-pressure gas cylinder; the rudder guide wings 14 are "X" guide wings.
In the invention, the aerial carrying platform comprises an autonomous flight aerial robot or a manned aircraft; the autonomous flight aviation robot includes unmanned helicopter, unmanned fixed wing airplane and unmanned remote control airship.
The structural characteristics, the working principle and the using process of the invention are described as follows:
the throwing fire extinguishing system and the guiding fire extinguishing system arranged on the aerial carrying platform can respectively complete different fire extinguishing tasks, wherein the throwing fire extinguishing system mainly realizes forest fire extinguishing and disaster relief; the throwing fire extinguishing system mainly realizes fire extinguishing and disaster relief of urban high-rise buildings.
Example 1:
forest fire extinguishing and relief work, if the road in the fire area is not smooth, the ground fire-fighting machinery is difficult to reach the fire area, and nearby water surface berths and fetches water which are not large enough, a load-carrying unmanned helicopter can be adopted to load a throwing fire-extinguishing system, the throwing fire-extinguishing system comprises a high-efficiency fire-fighting agent bag which is provided with a high-efficiency fire extinguishing agent and other fire extinguishing agents suitable for carrying, and the load-carrying unmanned helicopter flies to the sky above the fire area to extinguish fire at low altitude. If the fire area is great, can adopt the unmanned helicopter cluster of multiunit load to carry out the operation of putting out a fire, carry on large-scale free fall fire control bullet, throw through the unpowered free fall of annular throwing frame even symmetry and put out a fire, the purpose of even symmetry throwing is the gesture stable balance of guaranteeing aviation carrying platform. The throwing fire extinguishing system adopts a high-altitude physical throwing method, does not need powder power to push, and cannot generate new fire source hidden danger. The high-pressure air cylinder is an air cylinder with enough pressure and stores high-pressure air, the gravity impact control valve is firstly opened, the high-pressure air cylinder can release and guide the high-pressure air into the pressure air gathering cabin through the gravity impact control valve, the pressure air gathering cabin is a container with small bearing force and is made of hard paper materials and PVC thin materials, and the periphery of the pressure air gathering cabin is provided with an efficient fire extinguishing agent bag (fire extinguishing warhead) filled with efficient fire extinguishing agents. At the moment, the high-pressure air in the high-pressure air bottle is instantly gathered in the pressure air gathering cabin, when the air pressure reaches a high enough level, the cabin wall of the pressure air gathering cabin is exploded, and the surrounding high-efficiency fire extinguishing agent is thrown to surrounding fire areas, so that the purposes of fire extinguishing and disaster relief are achieved.
In order to ensure the balanced and stable posture of the aerial carrying platform, the free falling body fire-fighting bomb on the throwing frame must be symmetrically thrown by even number, and the whole throwing fire-extinguishing system is hung at the gravity center position of the aerial carrying platform and can freely swing for 360 degrees so as to overcome the influence of the change of load and mass center on the flying posture of the aerial carrying platform.
The throwing fire extinguishing system overcomes the problems of high operation cost, large human and machine risks and low fire extinguishing efficiency of the traditional manned helicopter, can realize cluster fire extinguishing operation by adopting a load-carrying unmanned helicopter, and is a scientific, safe, environment-friendly, low-consumption, high-efficiency, economic and feasible forest fire extinguishing and fire extinguishing system.
Example 2:
the urban high-rise building extinguishment and relief is a modernized urban fire-fighting operation problem, urban roads are increasingly blocked when high-rise buildings are built higher, the traditional fire-fighting operation surface cannot reach the height of a fire area, and the urban high-rise building extinguishment and relief task cannot be completed.
The thrust part is internally loaded with gunpowder, the thrust generated by the thrust part can enable the aviation guidance fire bomb to horizontally fly for about 50 meters and generally emit at a position which is no more than 20 meters away from a fire area, so that the hidden danger that secondary fire can be caused due to too large amount of gunpowder is avoided, the X-shaped guide wing can enable the aviation guidance fire bomb to guide and fly to the window of the fire area by utilizing the aerodynamic principle, the window breaking warhead is a conical warhead with certain strength, the window breaking is broken by utilizing the motion kinetic energy of the aviation guidance fire bomb to enter a building to reach the fire area, after the window breaking, a sensor on the high-pressure gas control valve immediately sends an instruction to open a gas valve, so that high-pressure air in a high-pressure gas cylinder is instantly gathered in the air gathering cabin, the principle is the same as that of the free-fall fire bomb, when the air pressure of the air gathering cabin is high enough, the pressure gathering part bursts at the, thereby achieving the purpose of extinguishing fire.
The guidance fire extinguishing system carried by the aerial carrying platform can not be influenced by ground traffic conditions, can timely and quickly arrive at a fire scene, accurately guides and launches fire-fighting missiles, timely, quickly and efficiently controls and eliminates disasters, overcomes the influence of ground fire extinguishing, disaster relief, fire fighting traffic jam, and solves the problems that fire extinguishing operation cannot reach disaster areas and heights, and fire extinguishing operation cannot be accurately carried out.
The above description is only an embodiment of the present invention, but the structural features of the present invention are not limited thereto, and the present invention can be applied to similar products, and any changes or modifications within the scope of the present invention by those skilled in the art are covered by the present invention.
Claims (7)
1. A high altitude aviation fire extinguishing and disaster relief system which characterized in that: comprises an aerial carrying platform, a throwing fire extinguishing system and a guidance fire extinguishing system which are arranged on the aerial carrying platform;
the throwing fire extinguishing system comprises an annular throwing frame and a plurality of free-falling body fire fighting bombs (1) arranged at the lower end of the annular throwing frame, the annular throwing frame is fixed at the central position below an aerial carrying platform, the annular throwing frame comprises suspension buckles (2), the upper ends of the suspension buckles (2) are connected below the aerial carrying platform, the lower ends of the suspension buckles (2) are connected with a plurality of connecting frame bodies (3), the lower ends of the plurality of connecting frame bodies (3) are connected with suspension ring frames (4), the suspension ring frames (4) are connected with a plurality of fire fighting bomb lifting ropes (5) at equal intervals, each fire fighting bomb lifting rope (5) is provided with an electronic lock catch (6), and the plurality of free-falling body fire fighting bombs (1) are connected with the respective fire fighting bomb lifting ropes (5) through the electronic lock catches (6);
guidance fire extinguishing systems is including launching cabin (7) and a plurality of pieces of aviation guidance fire control bullet (8) of setting in launching cabin (7), launching cabin (7) are single storehouse structure of erectting, including a plurality of year bomb cavity, and every carries and all establishes in the bomb cavity aviation guidance fire control bullet (8), is equipped with electronic lock and ignition control circuit in the launching cabin, and the launching cabin passes through universal ring (17) and connects the below of carrying on the platform in the air.
2. An aviation fire-fighting disaster-relief system according to claim 1, wherein: free fall fire control bullet (1) includes high-pressure cylinder (9), gravity striking control valve (10), pressurized air gathering cabin (11) and high-efficient fire extinguishing agent package (12), high-pressure cylinder (9) set up the afterbody at free fall fire control bullet (1), and the inside storage highly-compressed air of high-pressure cylinder (9), the front end of high-pressure cylinder (9) set up gravity striking control valve (10), and high-pressure cylinder (9) are through gravity striking control valve (10) and pressurized air gathering cabin (11) intercommunication, pressurized air gathering cabin (11) are the not big container structure of load, at the outside parcel of pressurized air gathering cabin (11) high-efficient fire extinguishing agent package (12).
3. An aerial fire-fighting disaster-relief system according to claim 1 or 2, characterized in that: the aviation guidance fire bomb (8) comprises a thrust part (13), a guidance rudder wing (14), a high-pressure gas cylinder (9), a high-pressure gas control valve (15), a pressure air gathering cabin (11), an efficient fire-fighting agent bag (12) and a window breaking warhead (16); guidance rudder wing (14) set up the afterbody at aviation guidance fire control bullet (8), thrust portion (13) set up the tail end in aviation guidance fire control bullet (8), the front end of thrust portion (13) sets up high-pressure gas cylinder (9), the inside storage highly-compressed air of high-pressure gas cylinder (9), the front end of high-pressure gas cylinder (9) sets up high-pressure gas control valve (15), high-pressure gas cylinder (9) gather cabin (11) intercommunication through high-pressure gas control valve (15) and pressure air, at high-efficient fire extinguishing agent package (12) of pressure air gathering cabin (11) outside parcel, broken window warhead (16) set up the end at aviation guidance fire control bullet (8).
4. An aviation fire-fighting disaster-relief system according to claim 3, wherein: the aerial embarkation platform comprises an autonomous flight aerial robot or a manned aircraft.
5. The fire fighting aviation system according to claim 4, wherein: the autonomous flight aerial robot comprises an unmanned helicopter, an unmanned fixed wing airplane and an unmanned remote control airship.
6. An aerial fire-fighting disaster-relief system according to claim 5, characterized in that: the guide rudder wing (14) is an X-shaped guide wing.
7. The fire fighting aviation system according to claim 6, wherein: the window breaking warhead (16) is a cone-shaped frame structure warhead and is arranged at the end of the aviation guidance fire-fighting bomb (8) through four rigid rods.
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CN202010356034.XA CN111589016A (en) | 2020-04-29 | 2020-04-29 | High-altitude aviation fire extinguishing and disaster relief system |
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Cited By (1)
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CN112960114A (en) * | 2021-02-04 | 2021-06-15 | 国家能源(山东)工程技术有限公司 | Fire control unmanned aerial vehicle |
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CN207734492U (en) * | 2017-12-11 | 2018-08-17 | 陈春霞 | Fire extinguisher bomb and its emission system |
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US20100065288A1 (en) * | 2008-09-12 | 2010-03-18 | Lonestar Inventions, L.P. | Vehicle for Aerial Delivery of Fire Retardant |
CN103691084A (en) * | 2014-01-17 | 2014-04-02 | 徐鹏 | Fire extinguishing device |
CN105270629A (en) * | 2015-11-06 | 2016-01-27 | 中国航空工业经济技术研究院 | System of forest fire fighting unmanned aircraft system |
CN207734492U (en) * | 2017-12-11 | 2018-08-17 | 陈春霞 | Fire extinguisher bomb and its emission system |
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CN112960114A (en) * | 2021-02-04 | 2021-06-15 | 国家能源(山东)工程技术有限公司 | Fire control unmanned aerial vehicle |
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Application publication date: 20200828 |
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