CN206138606U - Aircraft drives cigarette device for fire control - Google Patents
Aircraft drives cigarette device for fire control Download PDFInfo
- Publication number
- CN206138606U CN206138606U CN201621121781.0U CN201621121781U CN206138606U CN 206138606 U CN206138606 U CN 206138606U CN 201621121781 U CN201621121781 U CN 201621121781U CN 206138606 U CN206138606 U CN 206138606U
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- CN
- China
- Prior art keywords
- fire
- water pump
- aircraft
- aircraft body
- master control
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- 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.)
- Expired - Fee Related
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- Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
Abstract
The utility model belongs to the technical field of the fire prevention technique disappears and specifically relates to an aircraft drives cigarette device for fire control, including the aircraft main part, the top of aircraft main part is provided with signal transceiver, be provided with the bracing piece on the lateral wall of aircraft main part, the spout has been seted up in the bracing piece, the inboard bottom of aircraft main part is provided with the water tank, the water pump is connected with the water tank, flexible pipe is kept away from the one end of water pump and is connected with water spray bar, water spray bar is close to the both sides of flexible pipe and all installs the worm, be provided with initiative turbine and driven turbine in the install bin, the aircraft main part is close to the both sides of water pump and is all installed the support frame, the bottom and the micro motor of support frame are connected, one side of support frame is passed through the connecting rod and is connected with the install bin, micro motor is connected with the initiative turbine in the install bin. The utility model discloses simple structure, the personnel that will strand that can be quick rescue from the scene of a fire.
Description
Technical field
The utility model is related to fire control technology field, more particularly to a kind of drive cigarette device of fire-fighting aircraft.
Background technology
In recent years, the report of high-rise building with fire disaster is of common occurrence, once and these skyscraper occurrence of large-area fire
Calamity, the work of suing and labouring to trapped personnel will face great difficulty, often need to throw in relief goods or selfrescue equipment to trapped personnel,
Such as food, rope, life vest or rescue tool.But in high-rise building with fire disaster, due to the spaces such as room or corridor it is narrow
Little, a large amount of dense smokes also cause rescue site visibility relatively low, it is impossible to observe live the condition of a disaster, and trapped personnel also cannot be seen clearly to be thrown
The rescue articles for use position put, causes rescue work effectively to carry out, and delays rescue opportunity.Additionally, through investigation, finding most
Fire in high buildings casualty is because having sucked caused by a large amount of smog institutes.Containing great amount of carbon dioxide and some articles in smog
Toxic gas produced by burning, excessive suction can cause that people's is clouding of consciousness, escape ability be lost, accordingly, it would be desirable to a kind of fast
Prompt effectively escape method or rescue aid are ensureing the life security of trapped personnel.
Utility model content
The purpose of this utility model be in order to solve prior art in exist cannot observe the condition of a fire, can not be to the dense of the scene of a fire
Cigarette is driven away, and a kind of drive cigarette device of the fire-fighting aircraft for proposing.
To achieve these goals, the utility model employs following technical scheme：
A kind of drive cigarette device of fire-fighting aircraft, including aircraft body, are provided with the top of the aircraft body
Signal transceiver, is provided with support bar on the side wall of the aircraft body, and the upper end of support bar is provided with linear electric motors, institute
To state offered in support bar and be inserted with chute, and chute supporting leg, the supporting leg is connected with linear electric motors, the aircraft
The inside top of main body is provided with master control borad by buckle, and master control borad is electrically connected with linear electric motors, the downside of the master control borad
Electrical storage device is provided with, the electrical storage device is electrically connected respectively with linear electric motors and master control borad；
The inside bottom of the aircraft body is provided with water tank, and the aircraft body is offered near the bottom of water tank
Water pump is installed, the water pump is connected with water tank in through hole, and through hole, and water pump is electrically connected respectively with electrical storage device and master control borad
Connect, the delivery port of the water pump is connected with telescoping tube, the telescoping tube is connected away from one end of water pump with spray boom, the water spray
Some water jets are provided with bar, the spray boom is mounted on worm screw near the both sides of telescoping tube, and the worm screw is plugged in peace
In vanning, and the top of worm screw is provided with limited block through case is installed, and active turbine and driven whirlpool are provided with the installation case
Take turns, and active turbine and driven turbine wheel are connected with worm screw；
The aircraft body is mounted on bracing frame, the bottom of support frame as described above and micromachine near the both sides of water pump
Connect, and micromachine is electrically connected respectively with electrical storage device, master control borad, the side of support frame as described above is by connecting rod and installation case
Connection, the micromachine is connected with the active turbine in case is installed.
Preferably, the electrical storage device is battery.
Preferably, antenna is installed on the signal transceiver, and antenna is electrically connected with signal transceiver.
Preferably, the driven turbine wheel is connected by rotating shaft with the side wall for installing case.
Preferably, the water pump is provided with the rubber sheet gasket for preventing leak with the junction of telescoping tube.
Preferably, the bottom of the aircraft body is provided with the mounting blocks for mounting hook.
The utility model proposes a kind of fire-fighting aircraft drive cigarette device, beneficial effect is：When in use, by water
Case is filled after water, starts aircraft body, while linear electric motors are contracted to supporting leg in support bar, after the scene of a fire is flown to, is opened
Actuating miniature motor adjusts the angle of spray boom, and angle starts water pump after mixing up, and the smog in the scene of a fire is driven with the method for water spray
Dissipate, the utility model simple structure is easy to use, and quickly the smog in the scene of a fire can be dispersed, and quickly rescues trapped personnel.
Description of the drawings
Fig. 1 be the utility model proposes a kind of fire-fighting aircraft drive cigarette device structural representation：
Fig. 2 be the utility model proposes a kind of fire-fighting aircraft drive cigarette device installation case internal structure illustrate
Figure.
In figure：Supporting leg 1, bracing frame 2, support bar 3, linear electric motors 4, aircraft body 5, master control borad 6, signal transceiver
7th, electrical storage device 8, water tank 9, micromachine 10, worm screw 11, installation case 12, telescoping tube 13, water pump 14, spray boom 15, water jet
16th, limited block 17, active turbine 18, driven turbine wheel 19.
Specific embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is only a part of embodiment of the utility model, rather than whole
Embodiment.
With reference to Fig. 1-2, a kind of drive cigarette device of fire-fighting aircraft, including aircraft body 5, the top of aircraft body 5
Portion is provided with signal transceiver 7, and antenna is provided with signal transceiver 7, and antenna is electrically connected with signal transceiver 7, it is ensured that letter
Number stable, the bottom of aircraft body 5 is provided with the mounting blocks that can be used for mounting hook, and mounting hook transports rescue tool, flies
Support bar 3 is provided with the side wall of row device main body 5, and the upper end of support bar 3 is provided with linear electric motors 4, support bar 3 and offers
Supporting leg 1 is inserted with chute, and chute, supporting leg 1 is connected with linear electric motors 4, the inside top of aircraft body 5 is by card
Button is provided with master control borad 6, and master control borad 6 is electrically connected with linear electric motors 4, and the downside of master control borad 6 is provided with electrical storage device 8, electric power storage
Device 8 is battery, and power supply is stable, and electrical storage device 8 is electrically connected respectively with linear electric motors 4 and master control borad 6, it is ensured that stable,
Improve operating efficiency.
The inside bottom of aircraft body 5 is provided with water tank 9, and aircraft body 5 offers logical near the bottom of water tank 9
Water pump 14 is installed, water pump 14 is connected with water tank 9 in hole, and through hole, and water pump 14 is electric with electrical storage device 8 and master control borad 6 respectively
Connection, the delivery port of water pump 14 is connected with telescoping tube 13, and water pump 14 is provided with the rubber for preventing leak with the junction of telescoping tube 13
Glue gasket, telescoping tube 13 is connected away from one end of water pump 14 with spray boom 15, and some water jets 16 are provided with spray boom 15, spray
Water bar 15 is mounted on worm screw 11 near the both sides of telescoping tube 13, and worm screw 11 is plugged in installation case 12, and the top of worm screw 11
Limited block 17 is provided with through case 12 is installed, is installed in case 12 and is provided with active turbine 18 and driven turbine wheel 19, and active turbine
18 and driven turbine wheel 19 be connected with worm screw 11, driven turbine wheel 19 by rotating shaft with installation case 12 side wall be connected, it is possible to increase
The service life of the device.
Aircraft body 5 is mounted on bracing frame 2, bottom and the micromachine 10 of bracing frame 2 near the both sides of water pump 14
Connect, and micromachine 10 is electrically connected respectively with the master control borad 6 of electrical storage device 8, the side of bracing frame 2 is by connecting rod and installation case
12 connections, micromachine 10 is connected with the active turbine 18 in case 12 is installed, and spray boom 15 is adjusted by micromachine 10
Angle, the smog to the scene of a fire that accurate can lack passes through to spray water and evacuates, and the utility model simple structure is easy to use, can be quick
The smog to the scene of a fire disperse.
Workflow：When in use, water tank 9 is filled after water, starts aircraft body 5, while will by linear electric motors 4
Supporting leg 1 is contracted in support bar 3, after the scene of a fire is flown to, starts the angle that micromachine 10 adjusts spray boom 15, and angle is mixed up
Start water pump 14 afterwards, the smog in the scene of a fire is dispersed with the method for water spray, the utility model simple structure, easy to use, energy
It is enough that quickly the smog in the scene of a fire is dispersed, quickly rescue trapped personnel.
The above, only the utility model preferably specific embodiment, but protection domain of the present utility model is not
Be confined to this, any those familiar with the art in the technical scope that the utility model is disclosed, according to this practicality
New technical scheme and its utility model design in addition equivalent or change, all should cover in protection model of the present utility model
Within enclosing.
Claims (6)
1. a kind of drive cigarette device of fire-fighting aircraft, including aircraft body (5), it is characterised in that：The aircraft body
(5) signal transceiver (7) is provided with the top of, support bar (3) is provided with the side wall of the aircraft body (5), and supported
The upper end of bar (3) is provided with to be offered in linear electric motors (4), the support bar (3) and be inserted with chute, and chute supporting leg
(1), the supporting leg (1) is connected with linear electric motors (4), and the inside top of the aircraft body (5) is provided with by buckle
Master control borad (6), and master control borad (6) electrically connects with linear electric motors (4), and on the downside of the master control borad (6) electrical storage device is provided with
(8), the electrical storage device (8) electrically connects respectively with linear electric motors (4) and master control borad (6)；
The inside bottom of the aircraft body (5) is provided with water tank (9), and the aircraft body (5) is near the bottom of water tank (9)
Portion offers and be provided with through hole, and through hole water pump (14), and the water pump (14) is connected with water tank (9), and water pump (14) is respectively
Electrically connect with electrical storage device (8) and master control borad (6), the delivery port of the water pump (14) is connected with telescoping tube (13), it is described flexible
Pipe (13) is connected away from one end of water pump (14) with spray boom (15), and on the spray boom (15) some water jets are provided with
(16), the spray boom (15) is mounted on worm screw (11) near the both sides of telescoping tube (13), and the worm screw (11) is plugged in peace
In vanning (12), and the top of worm screw (11) is provided with limited block (17) through case (12) is installed, and sets in installation case (12)
Active turbine (18) and driven turbine wheel (19) are equipped with, and active turbine (18) and driven turbine wheel (19) are connected with worm screw (11)；
The aircraft body (5) is mounted on bracing frame (2), the bottom of support frame as described above (2) near the both sides of water pump (14)
It is connected with micromachine (10), and micromachine (10) is electrically connected respectively with electrical storage device (8), master control borad (6), support frame as described above
(2) side is connected by connecting rod with case (12) is installed, the active turbine in the micromachine (10) and installation case (12)
(18) connect.
2. the drive cigarette device of a kind of fire-fighting aircraft according to claim 1, it is characterised in that：The electrical storage device
(8) it is battery.
3. the drive cigarette device of a kind of fire-fighting aircraft according to claim 1, it is characterised in that：The signal transceiver
(7) antenna is installed on, and antenna is electrically connected with signal transceiver (7).
4. the drive cigarette device of a kind of fire-fighting aircraft according to claim 1, it is characterised in that：The driven turbine wheel
(19) it is connected with the side wall for installing case (12) by rotating shaft.
5. the drive cigarette device of a kind of fire-fighting aircraft according to claim 1, it is characterised in that：The water pump (14) with
The junction of telescoping tube (13) is provided with the rubber sheet gasket for preventing leak.
6. the drive cigarette device of a kind of fire-fighting aircraft according to claim 1, it is characterised in that：The aircraft body
(5) bottom is provided with the mounting blocks that can be used for mounting hook.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621121781.0U CN206138606U (en) | 2016-10-13 | 2016-10-13 | Aircraft drives cigarette device for fire control |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621121781.0U CN206138606U (en) | 2016-10-13 | 2016-10-13 | Aircraft drives cigarette device for fire control |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206138606U true CN206138606U (en) | 2017-05-03 |
Family
ID=58621807
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621121781.0U Expired - Fee Related CN206138606U (en) | 2016-10-13 | 2016-10-13 | Aircraft drives cigarette device for fire control |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206138606U (en) |
-
2016
- 2016-10-13 CN CN201621121781.0U patent/CN206138606U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170503 Termination date: 20191013 |