CN108744343A - A kind of fire-fighting mode - Google Patents
A kind of fire-fighting mode Download PDFInfo
- Publication number
- CN108744343A CN108744343A CN201810658023.XA CN201810658023A CN108744343A CN 108744343 A CN108744343 A CN 108744343A CN 201810658023 A CN201810658023 A CN 201810658023A CN 108744343 A CN108744343 A CN 108744343A
- Authority
- CN
- China
- Prior art keywords
- fire
- aircraft
- fighting
- safety rope
- pipeline
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
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Classifications
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/006—Safety devices
-
- 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
-
- 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
- A62C3/0242—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 by spraying extinguishants from the aircraft
-
- A—HUMAN NECESSITIES
- A62—LIFE-SAVING; FIRE-FIGHTING
- A62C—FIRE-FIGHTING
- A62C37/00—Control of fire-fighting equipment
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/16—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting
- B64D1/18—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting by spraying, e.g. insecticides
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F3/00—Ground installations specially adapted for captive aircraft
- B64F3/02—Ground installations specially adapted for captive aircraft with means for supplying electricity to aircraft during flight
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Emergency Management (AREA)
- Business, Economics & Management (AREA)
- Public Health (AREA)
- Health & Medical Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Ecology (AREA)
- Biodiversity & Conservation Biology (AREA)
- Forests & Forestry (AREA)
- Mechanical Engineering (AREA)
- Combustion & Propulsion (AREA)
- Chemical & Material Sciences (AREA)
- Remote Sensing (AREA)
- Pest Control & Pesticides (AREA)
- Emergency Lowering Means (AREA)
- Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
Abstract
The invention discloses a kind of skyscraper fire-fighting modes, it is characterised in that:Pipeline is carried using aircraft, the downward ejecting extinguishing medium fire extinguishing of pipeline is pulled from building, or utilize safety rope pull-up conducting wire or pipeline, the fire extinguishing of ejecting extinguishing substance.Method using the present invention can mitigate the load of aircraft, greatly increase the extinguishing ability of aircraft.
Description
Technical field
The invention belongs to fire-fighting domain, especially a kind of fire-fighting mode can be used in skyscraper fire extinguishing.
Background technology
In recent years, high-rise, high-rise building fire fighting problem getting worse, work all occurred for the ground such as Beijing, Shanghai, London
The fire of high-rise building of name.The consequence that skyscraper catches fire is very serious, and it is extremely difficult to be primarily due to its rescue.Currently, disappearing
The fire extinguishing height of anti-vehicle only has more than 100 meters, the height of about 30-50 floors, then high then helpless.
Applicant have observed that have fire water supply on the position that catches fire for building of catching fire, it therefore, can be at the first time
It is put out a fire using the water of the upper high potential energy of building, avoids causing the intensity of a fire to expand during waiting for fire fighting truck, loss is dropped to most
It is low.
Invention content
Goal of the invention:The present invention provides a kind of modes can be used for skyscraper fire extinguishing.
Technical scheme is as follows:
Certain firing-fighting medium is usually stored in building or keeps to provide the energy of firing-fighting medium in building at any time
Power, such as using fire water box water storage or fire protection pipeline is built, it can utilize fire pump will by fire protection pipeline at any time
The firing-fighting mediums such as water, foam transport building top.
Preferably, certain firing-fighting medium can be stored in the top area of building or keep at any time can be to building
Build the ability that top provides firing-fighting medium.The building top refer to build half height more than floor or building the 10th layer with
On floor.Simultaneously prepare some tubes building top area.The tube is used for transporting firing-fighting medium, including but
It is not limited to water pipe, water band.
As further preferred, the roof that can be built stores certain firing-fighting medium or keep at any time can be to building
Build the ability that top provides firing-fighting medium.
Meanwhile preparing an aircraft, the aircraft contains motor, rotor, control unit, rack;The rotor
It it is 2 or 2 or more, the control unit includes but not limited to fly control, electron speed regulator, receiver.
Preferably, in order to further enhance the safety of aircraft, safety rope, Huo Zhefei can be installed on board the aircraft
The interface that can install safety rope is reserved on row device or in the rack of aircraft.One fixation of safety rope is on board the aircraft;
Other end is fixed on except aircraft, is generally fixed to eminence.The pulling force that safety rope can be born is more than 100N or more.Described
Safety rope is including but not limited to steel wire rope, elastic string.
As further preferred, M kilograms also bigger than the quality of aircraft of the quality of the load that safety rope can be born with
On, the range of M is 20 ~ 5000 kilograms.
As further preferred, bobbin winder device folding and unfolding safety rope may be used, to control the length and aircraft of safety rope
Position mutually coordinate, ensure to hold in time when aircraft falls, being unlikely to fall too, decrease speed is too fast long afterwards.For example, can
Folding and unfolding to control steel wire rope as safety rope, using electric block using steel wire rope.
Safety rope is bound together with tube near aircraft preferably, fixture may be used.Essence in this way
To utilize safety rope pull-up tube, to mitigate the burden of aircraft, conducting wire, tube most of weight all held by safety rope
By aircraft only needs to bear the weight of seldom safety rope, tube, and aircraft has the load capacity of bigger to go to put out a fire.
The fire-fighting mode of the present invention is as follows:
After a certain floor of building catches fire, water pipe, water band etc. can be transported to tube one end of firing-fighting medium in building
It is connected to the firing-fighting medium source on roof, the other end is fixed on aircraft, and connects nozzle or nozzle.
Safety rope is such as used, the both ends of safety rope are connected firmly with the secured place of roof equal-height position, aircraft frame respectively,
For example, can building top be mounted on electric block, the steel wire rope on electric block is fixed on aircraft;
After connecting, aircraft takeoff is controlled, and is usually to fly down(Because position when taking off is higher), fire extinguishing position of flying to
It sets.In this way, aircraft can be put out a fire with ejecting extinguishing medium.
The present invention can also use following fire-fighting mode:
Safety rope is fixed in building, and firing-fighting medium source, tube, aircraft are all placed and ground, aircraft is on ground
Tube, safety rope are connected, while being tied up safety rope and one or two of pipeline, conducting wire near aircraft using fixture
It is scheduled on together.Essence is to utilize one or two of safety rope pull-up pipeline, conducting wire in this way, to mitigate the burden of aircraft,
Conducting wire, pipeline, safety rope most of weight all born by safety rope, aircraft only need to bear seldom conducting wire, safety rope,
The weight of pipeline, aircraft have the load capacity of bigger to go to carry out other work.
Tube, control aircraft flight, fire extinguishing are sling using safety rope in this way.Its advantage is that tube and firing-fighting medium
Most of weight can be born by safety rope, and it is more convenient in terrestrial operation.
The transformation of other similar fire-fighting modes based on the present invention, all within protection scope of the present invention.
The fire-fighting mode of the present invention has following feature:The fire-fighting mode carries pipeline using aircraft, from high potential energy
Firing-fighting medium, the fire extinguishing of ejecting extinguishing medium are transported at firing-fighting medium source;Or fix safety rope aloft, it is drawn using safety rope
Play the fire extinguishing of duct injection firing-fighting medium.
As can be seen that the position when extreme lower position when aircraft flight of the present invention can set out less than it, Huo Zhefei
2 meters lower than the peak of safety rope of minimum altitude when row device flight or more.
Preferably, also covering the rotor of the aircraft in the present invention using guard, other objects are met to prevent the spin-ended wing
Body.
Preferably, nozzle or nozzle can be installed on tube, irrigation pressure is improved.
Beneficial effect:
There are two important innovative points by the present invention:1. current fire fighting truck is all that the firing-fighting mediums such as water, foam is sent to put out a fire from the bottom up,
And the aircraft of the present invention usually send firing-fighting medium to put out a fire from the top down;2. current flight device is usually upward flight operation,
And the theory of the present invention is that downward flight operation may be used in aircraft.
Certainly, this aircraft also has the ability of up flight operation.
The two innovative points give the advantage that:
1. using the aircraft of the present invention program, by aircraft pull-up pipeline, put out a fire downwards from eminence transport firing-fighting medium, from
And high-rise, any floor of high-rise building the fire that can go out, much breaching current fire fighting truck can only go out more than 100 meters of high building
Limitation, the world-famous puzzle that thoroughly radical cure is high-rise, high-rise building fire extinguishing is difficult;
2. since safety rope can bear larger pulling force, and it is fixed aloft, avoid aircraft and directly drop into ground and make
At consequence, be a kind of safe equipment;
3. due to all fixations of safety rope, pipeline or quoted from eminence, in this way, most of weight of safety rope, pipeline is by their own
It bears, aircraft only needs to bear few moiety by weight, has the load capacity of bigger to go work in this way.
In addition, the fire-fighting of the present invention can be put out a fire with rescue system from all angles, such as left and right, upper and lower side
Position.The building on periphery can also carry out joint fire-fighting.The cost of the present invention is also very cheap.
To facilitate the understanding of the present invention, accompanying drawings and embodiments are provided below for explaining the present invention, but they are not constituted pair
The restriction of the present invention.
Description of the drawings
Fig. 1 is the aircraft fire extinguishing schematic diagram of the present invention.
Reference sign:
1- aircraft
3- rubber water pipes
6- carbon fiber pipes
16- safety ropes
The connection relationship diagram of Fig. 2 aircraft of the present invention and water pipe.
Reference sign:
3- rubber water pipes
6- carbon fiber water pipes
11- racks
12- rotors
13- motors
14- guards
16- safety ropes
17- arms
18- tripods
Fig. 3 is the structural schematic diagram of electric block.
Reference sign:
16- safety ropes
20- cantilevers
22- columns
23- pedestals
24- pulleys
27- motors
28- controllers
29- reels
Fig. 4 is safety rope, water pipe binding schematic diagram.
Reference sign:
1- aircraft
3- water pipes
20- cantilevers
22- columns
23- pedestals
24- pulleys
27- motors
28- controllers
29- reels
26- safety ropes
Specific implementation mode
Below by detailed description of the present invention fire fighting mode in conjunction with the embodiments.
Embodiment 1
Schematic diagram of putting out a fire is as shown in Figure 1.Aircraft 1 uses a diameter of 16 using hundred million 184 rotor type aircraft of boat, safety rope 16
The steel wire rope of millimeter, tube 3 uses internal diameter for 50 millimeters, the rubber water pipe of the steel wire reinforcement of 54 millimeters of outer diameter, in robber cement
54 millimeters of internal diameter, 2 millimeters of wall thickness, long 1.5 meters of carbon fiber pipe 6 are connected on pipe, and carbon fiber pipe is fixed on aircraft 1.Rubber
The other end of tube of glue connects the water outlet of fire hydrant on roof and fixation.
Specifically, the position of the water inlet of carbon fiber pipe is fixed on close to aircraft center of gravity position, as shown in Figure 2.Again
Nozzle is installed in carbon fiber nozzle.
Before flight, by electric block(Fig. 3)It is fixed on roofdeck edge, lay winding wire ropes on the reel 29 of electric block
(Safety rope)16, safety rope 16 hangs down along external wall to be fallen to the ground, and is fixed one end of safety rope 16 using retainer clip
Near the position of centre of gravity of aircraft.In this way, when aircraft flies up, safety rope can be adjusted by controlling electric block
Length.Once aircraft is out of control, aircraft can be held, be unlikely to Crater face by safety rope.
In this way, taken off with remote control control aircraft 1, open fire hydrant valve, then aircraft 1 can pull-up water pipe water spray go out
Fire.
Embodiment 2
As shown in figure 4, on the basis of embodiment 1, further, using fixture by safety rope 16 and conducting wire 15, robber cement
Pipe 5 is bound together at separate 20 meters of aircraft.In this way, most of weight of conducting wire, safety rope, water pipe is all held by safety rope
By aircraft has the load capacity of bigger to go to carry out fire-fighting work.
The above is only two examples of embodiment of the present invention, it should be pointed out that:For the technology people of the art
For member, various improvements and modifications may be made without departing from the principle of the present invention, these improvements and modifications are also answered
It is considered as protection scope of the present invention.
Claims (5)
1. a kind of fire-fighting mode, it is characterised in that:The fire-fighting mode carries pipeline using aircraft, from the firing-fighting medium in building
Firing-fighting medium, the fire extinguishing of ejecting extinguishing medium are transported at source, or safety rope is fixed in building, utilize safety rope pull-up pipeline
Ejecting extinguishing medium is put out a fire;The load that the safety rope can bear the pulling force of 100N or more or the safety rope can be born
For quality than also big M kilograms or more of the quality of aircraft, the range of M is 20 ~ 5000.
2. a kind of fire-fighting mode as described in claim 1, it is characterised in that:The aircraft used in the fire-fighting mode contains 2
A or 2 or more rotors.
3. a kind of fire-fighting mode as described in claim 1, it is characterised in that:The safety rope used in the fire-fighting mode include but
It is not limited to steel wire rope.
4. a kind of fire-fighting mode as described in claim 1, it is characterised in that:Tube one end is connected to roof in building
Firing-fighting medium source, the other end is fixed on aircraft, and connects nozzle or nozzle on pipeline, electric block is mounted on and is built
It builds, the steel wire rope on electric block is connected firmly in the rack of aircraft, control aircraft takeoff, go to fire extinguishing.
5. a kind of fire-fighting mode as described in claim 1, it is characterised in that:Electric block is mounted in building, it will be electronic
Steel wire rope on cucurbit is connected firmly in the rack of the aircraft on ground, and tube one end, which is connected to fire extinguishing, on ground is situated between
Matter source, the other end are fixed on aircraft, while being tightened steel wire rope and pipeline using fixture, and pipeline is enable to be hung in steel wire rope
On, and nozzle or nozzle are connected on pipeline, aircraft takeoff is controlled, fire extinguishing is gone to.
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201720748168 | 2017-06-26 | ||
CN201720748168X | 2017-06-26 | ||
CN201721028807 | 2017-08-17 | ||
CN2017210288071 | 2017-08-17 |
Publications (1)
Publication Number | Publication Date |
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CN108744343A true CN108744343A (en) | 2018-11-06 |
Family
ID=63976730
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
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CN201810658024.4A Pending CN108791834A (en) | 2017-06-26 | 2018-06-25 | A kind of fire-fighting aircraft and its fire-fighting mode |
CN201810658023.XA Pending CN108744343A (en) | 2017-06-26 | 2018-06-25 | A kind of fire-fighting mode |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
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CN201810658024.4A Pending CN108791834A (en) | 2017-06-26 | 2018-06-25 | A kind of fire-fighting aircraft and its fire-fighting mode |
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CN (2) | CN108791834A (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
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CN110251862A (en) * | 2019-06-20 | 2019-09-20 | 中国十七冶集团有限公司 | A kind of fire detection suppression system based on unmanned air vehicle technique |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101574565A (en) * | 2009-06-25 | 2009-11-11 | 北京大业嘉成科技有限公司 | Ducted fan flexible aerial ladder fire truck |
CN102107734A (en) * | 2009-12-23 | 2011-06-29 | 纳耶夫·宾马姆杜·宾阿卜杜尔阿齐兹阿尔沙特 | Helicopter to which fire-fighting and rescue facility can be attached and connected |
CN203790491U (en) * | 2014-03-25 | 2014-08-27 | 沈有宁 | High-rise building fire extinguishing device |
CN106379554A (en) * | 2016-12-08 | 2017-02-08 | 中国科学院长春光学精密机械与物理研究所 | Flight test protection device and method |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN204606235U (en) * | 2015-05-04 | 2015-09-02 | 厦门大学 | Many rotor wing unmanned aerial vehicles device when navigating based on the length hanging mooring system |
-
2018
- 2018-06-25 CN CN201810658024.4A patent/CN108791834A/en active Pending
- 2018-06-25 CN CN201810658023.XA patent/CN108744343A/en active Pending
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101574565A (en) * | 2009-06-25 | 2009-11-11 | 北京大业嘉成科技有限公司 | Ducted fan flexible aerial ladder fire truck |
CN102107734A (en) * | 2009-12-23 | 2011-06-29 | 纳耶夫·宾马姆杜·宾阿卜杜尔阿齐兹阿尔沙特 | Helicopter to which fire-fighting and rescue facility can be attached and connected |
CN203790491U (en) * | 2014-03-25 | 2014-08-27 | 沈有宁 | High-rise building fire extinguishing device |
CN106379554A (en) * | 2016-12-08 | 2017-02-08 | 中国科学院长春光学精密机械与物理研究所 | Flight test protection device and method |
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CN108791834A (en) | 2018-11-13 |
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Application publication date: 20181106 |
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