CN208339950U - A kind of high building fire fighting aviation mechanism - Google Patents
A kind of high building fire fighting aviation mechanism Download PDFInfo
- Publication number
- CN208339950U CN208339950U CN201820148637.9U CN201820148637U CN208339950U CN 208339950 U CN208339950 U CN 208339950U CN 201820148637 U CN201820148637 U CN 201820148637U CN 208339950 U CN208339950 U CN 208339950U
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- fire fighting
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- building fire
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- 230000007246 mechanism Effects 0.000 title claims abstract description 101
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 116
- 238000005507 spraying Methods 0.000 claims abstract description 34
- 230000000284 resting effect Effects 0.000 claims abstract description 4
- 239000007921 spray Substances 0.000 claims description 21
- 230000005611 electricity Effects 0.000 claims description 2
- 238000005286 illumination Methods 0.000 claims description 2
- 238000005259 measurement Methods 0.000 claims 1
- 238000000034 method Methods 0.000 description 4
- 238000010586 diagram Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000009435 building construction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 230000001535 kindling effect Effects 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 239000008400 supply water Substances 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
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- Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
- Special Spraying Apparatus (AREA)
Abstract
This application provides a kind of high building fire fighting aviation mechanisms, including Flight main body, water supply mechanism, cable, and the water spraying mechanism on the Flight main body is set, aerial control module, power module, camera, supersonic range finder, lighting system and counter-force mechanism, the water supply mechanism is rest on the ground, the water supply mechanism is connected by water supplying pipe with the water spraying mechanism, the water spraying mechanism, camera and, supersonic range finder, lighting system and counter-force mechanism are electrically connected with the aerial control module, the water spraying mechanism, aerial control module, camera, supersonic range finder, lighting system and counter-force mechanism are electrically connected with the power module, the power module is connect by cable with the power supply resting on the ground.High building fire fighting aviation mechanism provided by the present application, can fire extinguishing rapidly and efficiently, reduce loss.
Description
Technical field
The utility model relates to a kind of unmanned plane and fire-extinguishings, more particularly to a kind of high building fire fighting aviation mechanism.
Background technique
With the development of the social economy, building construction is higher and higher, in fire-fighting domain, high level fire extinguishing is always one
World-famous puzzle, the fire risk of skyscraper and fire extinguishing difficulty are far longer than general low-rise building, for fire source 100 meters with
On skyscraper, higher floor can not be arrived at fire fighting truck by commonly transporting to, and the speed that fireman reaches kindling place is slower
And be easy to miss best fire extinguishing reality, when that specifically cannot determine fire source place, it is also necessary to it is continuous artificially to find, not only waste
Time, and a large amount of physical strength of fire fighter can be wasted, if corresponding high level position does not have corresponding equipment that can directly use,
Task cannot be not only completed, can also increase casualties on foot, the robot of fire-fighting can be carried out in high-altitude if there is a kind of, and operate
It is all convenient with supplying water, very important effect can be played in fire extinguishing and rescue.
Utility model content
The purpose of the utility model is to provide a kind of high building fire fighting aviation mechanisms, and it is tired to solve high building fire fighting
Difficulty supplies water the problems such as inconvenient.
In order to solve the above technical problems, the utility model provides the following technical solutions:
A kind of high building fire fighting aviation mechanism, including Flight main body, water spraying mechanism, water supply mechanism, aerial control module,
Power module, camera, supersonic range finder, cable, lighting system and counter-force mechanism, it is the water spraying mechanism, aerial
Control module, power module, camera, supersonic range finder, lighting system and counter-force mechanism are arranged at described fly
In row main body, the water supply mechanism is arranged on the chassis on ground, and the Flight main body can be parked in the chassis
On top plate, the water supply mechanism is connected by water supplying pipe with the water spraying mechanism, the water spraying mechanism, camera, ultrasonic wave
Range unit, lighting system and counter-force mechanism are electrically connected with the aerial control module, the water spraying mechanism, aerial control
Molding block, camera, supersonic range finder, lighting system and counter-force mechanism are electrically connected with the power module, institute
Power module is stated to connect by cable with the power supply resting on the ground.
Further, the water spraying mechanism includes small-power water pump, hose, spray head, pipe collar, link block and driving machine
Structure, the small-power water pump are fixed on the Flight main body, the water inlet and the water supplying pipe of the small-power water pump
One end connection, the water outlet of the small-power water pump connect by the hose with the spray head, the hose it is close
One end of the spray head is equipped with pipe collar, and the pipe collar is bolted to connection on the link block, the driving machine
Structure makes the spray head swing for driving the link block to rotate.
Further, the driving mechanism includes gear, rack gear and electric pushrod, and the gear is articulated in the flight
In main body, the link block is fixedly and coaxially connected with the gear, and the rack gear is slidably arranged on the Flight main body, described
Rack gear is engaged with the gear, and the electric pushrod is fixed on the Flight main body, and the electric pushrod is flexible
Bar is fixedly connected with one end of the rack gear.
Further, the water supply mechanism includes high powered water pump, valve block and pressure gauge, the high powered water pump into
The mouth of a river is connected with water source, and the water outlet of the high powered water pump is connect by the valve block with the other end of the water supplying pipe,
The pressure gauge is arranged in the valve block.
Further, the Flight main body includes the first platform and is fixed on the upper surface of first platform
The second platform, the lower end surface of first platform is equipped with several supporting legs, if the upper surface of second platform is equipped with
The first motor of an annular spread is done, is fixedly connected with a propeller on the output shaft of each first motor.
Further, the water spraying mechanism, aerial control module and power module are arranged at first platform
On upper surface, and the water spraying mechanism, aerial control module and power module are respectively positioned on the lower section of second platform.
Further, the bottom surface of the supporting leg is equipped with cushion.
Further, the camera is fixed on second platform, and the camera is located at the spray
Drench the surface of head.
Further, the supersonic range finder is fixed on the bottom surface of first platform, for measuring
The flying height of the Flight main body.
Further, the counter-force mechanism includes the second motor and fan, and second motor is fixed at institute
It states on Flight main body, second motor is electrically connected with the aerial control module, power module, the fan and described second
The output shaft of motor is fixedly connected, and the fan can balance the recoil generated when water spraying mechanism work when rotating.
It can be seen from above-mentioned technical proposal the utility model has the following beneficial effects:
1. specified altitude assignment can quickly be reached using controlling remote control Flight main body, and fire source is quickly found, thus energy
It is enough quickly to determine ignition point, shorten rescue time;
2. since the water supplying pipe to supply water for water spraying mechanism is directly connect with surface pond, during avoiding fire-fighting, water is not
The problem of foot, while the weight of aviation mechanism is reduced, inertia is small, and it is easy to operate, so that fire-fighting process is easy, is convenient.
3. due to being equipped with counter-force mechanism, it is thus possible to balance recoil when water spraying mechanism work, Flight main body flies
Row process is steady.
The utility model is described in further detail with reference to the accompanying drawings and detailed description.
Detailed description of the invention
In order to illustrate the embodiment of the utility model or the technical proposal in the existing technology more clearly, below will be to embodiment
Or attached drawing needed to be used in the description of the prior art is briefly described, it should be apparent that, the accompanying drawings in the following description is only
It is the embodiments of the present invention, for those of ordinary skill in the art, without creative efforts, also
Other attached drawings can be obtained according to the attached drawing of offer.
Fig. 1 is the schematic perspective view of the utility model.
Fig. 2 is the water spraying mechanism of the utility model and the connection schematic diagram of water supply mechanism.
Fig. 3 is the structural schematic diagram of the water spraying mechanism of the utility model.
Description of symbols: Flight main body 1, supporting leg 11, cushion 111, the first platform 12, second the 13, first electricity of platform
Machine 14, propeller 15, water spraying mechanism 2, small-power water pump 21, hose 22, spray head 23, pipe collar 24, link block 25, gear 26,
Rack gear 27, water supply mechanism 3, high powered water pump 31, valve block 32, pressure gauge 33, water supplying pipe 34, controls mould at electric pushrod 28 in the air
Block 4, power module 5, camera 6, supersonic range finder 7, cable 8, lighting system 9, counter-force mechanism 10, the second motor
101, fan 102, chassis 100, bottom connecting plate 110, column 120, top plate 130, ground control module 200.
Specific embodiment
The embodiments of the present invention are described in detail below in conjunction with attached drawing, but the utility model can be by right
It is required that the multitude of different ways for limiting and covering is implemented.
The application is described further below with reference to Fig. 1 to Fig. 3, a kind of high building fire fighting flight as shown in Figure 1
Mechanism, including Flight main body 1, water spraying mechanism 2, water supply mechanism 3, aerial control module 4, power module 5, camera 6, ultrasonic wave
Range unit 7, cable 8, lighting system 9 and counter-force mechanism 10, the water spraying mechanism 2, aerial control module 4, power supply mould
Block 5, camera 6, supersonic range finder 7, lighting system 9 and counter-force mechanism 10 are arranged on the Flight main body 1,
The water supply mechanism 3 is arranged on the chassis 100 on ground, and the Flight main body 1 can be parked in the top of the chassis 100
On plate 130, the water supply mechanism 3 is connected by water supplying pipe 34 with the water spraying mechanism 2, the water spraying mechanism 2, camera 6,
Supersonic range finder 7, lighting system 9 and counter-force mechanism 10 are electrically connected with the aerial control module 4, the water spray
Mechanism 2, aerial control module 4, camera 6, supersonic range finder 7, lighting system 9 and counter-force mechanism 10 with it is described
Power module 5 is electrically connected, and the power module 5 is connect by cable 8 with the power supply resting on the ground, and the lighting system 9 is used
In providing illumination, camera 6 is enable clearly to shoot ambient enviroment.
As shown in Figure 1, the chassis 100 further includes bottom connecting plate 110 and several columns 120, the top plate 130 passes through
The column 120 is fixedly connected on the bottom connecting plate 110.
As shown in Fig. 2, the water spraying mechanism 2 includes small-power water pump 21, hose 22, spray head 23, pipe collar 24, link block
25 and driving mechanism, the small-power water pump 21 be fixed on the Flight main body 1, the water inlet of the small-power water pump 21
Mouth is connect with one end of the water supplying pipe 34, and the water outlet of the small-power water pump 21 passes through the hose 22 and the spray head
One end close to the spray head 23 of 23 connections, the hose 22 is equipped with pipe collar 24, and the pipe collar 24 is bolted
It is connected on the link block 25, the driving mechanism makes the spray head 23 for driving the link block 25 to rotate
It swings in the horizontal plane, increases water spray area, wherein the small-power water pump 21 and the aerial control module 4, power supply
Module 5 is electrically connected.
As shown in figure 3, the driving mechanism includes gear 26, rack gear 27 and electric pushrod 28, the gear 26 is articulated in
On the Flight main body 1, the link block 25 is fixedly and coaxially connected with the gear 26, and the rack gear 27 is slidably arranged in described
On Flight main body 1, the rack gear 27 is engaged with the gear 26, and the electric pushrod 28 is fixed at the Flight main body 1
On, and the telescopic rod of the electric pushrod 28 is fixedly connected with one end of the rack gear 27, the electric pushrod 28 and the sky
Middle control module 4, power module 5 are electrically connected.The telescopic rod of the electric pushrod 28, which is back and forth stretched out and shunk, drives the tooth
26 reciprocally swingings are taken turns, and then drive 25 reciprocally swinging of link block, finally make the spray head 23 left and right pendulum in the horizontal plane
It is dynamic.Using above-mentioned driving mechanism, drive process laborsaving, and reliable.
As shown in Fig. 2, the water supply mechanism 3 includes high powered water pump 31, valve block 32 and pressure gauge 33, the high-power water
Pump 31 is fixed on the bottom connecting plate 110 of the chassis 100, and the high powered water pump 31 be located at the chassis 100
On ground control module 200, the power electric connection that rest on the ground, the water inlet of the high powered water pump 31 is connected with water source
Logical, the water outlet of the high powered water pump 31 is connect by the valve block 32 with the other end of the water supplying pipe 34, the pressure
Table 33 is arranged in the valve block 32, and the pressure gauge 33 is used to detect the water pressure being located in the water supplying pipe 34, in turn
Judgement is located at the water level height of the water in the water supplying pipe 34, and water column overshoot is avoided to keep aviation mechanism unstable in flight course,
Also avoid the excessive appearance of pressure in water supplying pipe 34 dangerous.
As shown in Figure 1, the Flight main body 1 includes the first platform 12 and the upper end for being fixed at first platform 12
The second platform 13 on face, the lower end surface of first platform 12 are equipped with several supporting legs 11, on the bottom surface of the supporting leg 11
Equipped with cushion 111, avoid being equipped with several rings with rigid impact when supporting face contact, the upper surface of second platform 13
The first motor 14 of shape distribution, is fixedly connected with a propeller 15 on the output shaft of each first motor 14;The water spraying mechanism
2, aerial control module 4 and power module 5 are arranged on the upper surface of first platform 12, and the water spraying mechanism 2, sky
Middle control module 4 and power module 5 are respectively positioned on the lower section of second platform 13, reduce the center of gravity of aviation mechanism, stationarity
It is good.The first motor 14 is electrically connected with the aerial control module 4, power module 5.
As shown in Fig. 2, the camera 6 is fixed on second platform 13, and the camera 6 is positioned at described
The surface of spray head 23, the jet angle for the fire source adjustment spray head 23 that aerial control module 4 is monitored according to the camera 6
Degree, it is ensured that the fire location monitored is synchronous with eject position, improves fire-fighting efficiency;The fixation of supersonic range finder 7 is set
It sets on the bottom surface of first platform 12, for measuring the flying height of the Flight main body 1.
As shown in Fig. 2, the counter-force mechanism 10 includes the second motor 101 and fan 102, second motor 101
It being fixed on the Flight main body 1, second motor 101 is electrically connected with the aerial control module 4, power module 5,
The fan 102 is fixedly connected with the output shaft of second motor 101, and the fan 102 can balance the spray when rotating
The recoil that water dispenser structure 2 generates when working.
The flying height of the aviation mechanism of the application is 200m.
The above is only the preferred embodiments of the utility model, are not intended to limit the utility model, for this field
Technical staff for, various modifications and changes may be made to the present invention.Within the spirit and principle of the utility model,
Any modification, equivalent replacement, improvement and so on should be included within the scope of protection of this utility model.
Claims (10)
1. a kind of high building fire fighting aviation mechanism, which is characterized in that including Flight main body (1), water spraying mechanism (2), water supplying machine
Structure (3), aerial control module (4), power module (5), camera (6), supersonic range finder (7), cable (8), illumination system
System (9) and counter-force mechanism (10), the water spraying mechanism (2), aerial control module (4), power module (5), camera
(6), supersonic range finder (7), lighting system (9) and counter-force mechanism (10) are arranged on the Flight main body (1),
The water supply mechanism (3) is arranged on the chassis on ground (100), and the Flight main body (1) can be parked in the chassis
(100) on top plate (130), the water supply mechanism (3) is connected by water supplying pipe (34) with the water spraying mechanism (2), described
Water spraying mechanism (2), camera (6), supersonic range finder (7), lighting system (9) and counter-force mechanism (10) with it is described
Aerial control module (4) electrical connection, the water spraying mechanism (2), aerial control module (4), camera (6), ultrasonic distance measurement dress
It sets (7), lighting system (9) and counter-force mechanism (10) to be electrically connected with the power module (5), the power module (5)
It is connect by cable (8) with the power supply resting on the ground.
2. high building fire fighting aviation mechanism according to claim 1, which is characterized in that the water spraying mechanism (2) includes
Small-power water pump (21), hose (22), spray head (23), pipe collar (24), link block (25) and driving mechanism, the small-power water
Pump (21) is fixed on the Flight main body (1), the water inlet of the small-power water pump (21) and the water supplying pipe (34)
One end connection, the water outlet of the small-power water pump (21) connect by the hose (22) with the spray head (23), institute
The one end close to the spray head (23) for stating hose (22) is equipped with pipe collar (24), pipe collar (24) company of being bolted
It connects on the link block (25), the driving mechanism makes the spray head for driving the link block (25) to rotate
(23) it swings.
3. high building fire fighting aviation mechanism according to claim 2, which is characterized in that the driving mechanism includes gear
(26), rack gear (27) and electric pushrod (28), the gear (26) are articulated on the Flight main body (1), the link block
(25) it is fixedly and coaxially connected with the gear (26), the rack gear (27) is slidably arranged on the Flight main body (1), the tooth
Item (27) is engaged with the gear (26), and the electric pushrod (28) is fixed on the Flight main body (1), and the electricity
The telescopic rod of dynamic push rod (28) is fixedly connected with one end of the rack gear (27).
4. high building fire fighting aviation mechanism according to claim 2, which is characterized in that the water supply mechanism (3) includes
The water inlet of high powered water pump (31), valve block (32) and pressure gauge (33), the high powered water pump (31) is connected with water source, institute
The water outlet for stating high powered water pump (31) is connect by the valve block (32) with the other end of the water supplying pipe (34), the pressure
Table (33) is arranged on the valve block (32).
5. high building fire fighting aviation mechanism according to claim 2, which is characterized in that the Flight main body (1) includes
First platform (12) and the second platform (13) being fixed on the upper surface of first platform (12), first platform
(12) lower end surface is equipped with several supporting legs (11), and the upper surface of second platform (13) is equipped with several annular spreads
First motor (14), be fixedly connected with a propeller (15) on the output shaft of each first motor (14).
6. high building fire fighting aviation mechanism according to claim 5, which is characterized in that the water spraying mechanism (2), aerial
Control module (4) and power module (5) are arranged on the upper surface of first platform (12), and the water spraying mechanism (2),
Aerial control module (4) and power module (5) are respectively positioned on the lower section of second platform (13).
7. high building fire fighting aviation mechanism according to claim 5, which is characterized in that on the bottom surface of the supporting leg (11)
Equipped with cushion (111).
8. high building fire fighting aviation mechanism according to claim 5, which is characterized in that camera (6) fixation is set
It sets on second platform (13), and the camera (6) is located at the surface of the spray head (23).
9. high building fire fighting aviation mechanism according to claim 5, which is characterized in that the supersonic range finder
(7) it is fixed on the bottom surface of first platform (12), for measuring the flying height of the Flight main body (1).
10. high building fire fighting aviation mechanism according to claim 1, which is characterized in that the counter-force mechanism
It (10) include the second motor (101) and fan (102), second motor (101) is fixed at the Flight main body (1)
On, second motor (101) is electrically connected with the aerial control module (4), power module (5), the fan (102) and institute
The output shaft for stating the second motor (101) is fixedly connected, and the fan (102) can balance the water spraying mechanism (2) work when rotating
As when the recoil that generates.
Priority Applications (1)
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CN201820148637.9U CN208339950U (en) | 2018-01-29 | 2018-01-29 | A kind of high building fire fighting aviation mechanism |
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CN201820148637.9U CN208339950U (en) | 2018-01-29 | 2018-01-29 | A kind of high building fire fighting aviation mechanism |
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
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CN109823545A (en) * | 2019-03-27 | 2019-05-31 | 河南机电职业学院 | A kind of injection recoil force eliminating device and removing method for hybrid power unmanned plane |
CN110339515A (en) * | 2019-08-02 | 2019-10-18 | 张廷建 | Pneumatic power flight robot fire-fighting system and the method put out a fire using the system |
CN111529993A (en) * | 2020-04-29 | 2020-08-14 | 中国民用航空飞行学院 | Be applied to unmanned aerial vehicle's suspension extinguishing device |
CN112370689A (en) * | 2019-10-28 | 2021-02-19 | 周丽娟 | Novel communication wire and cable fire extinguishing unmanned aerial vehicle |
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2018
- 2018-01-29 CN CN201820148637.9U patent/CN208339950U/en not_active Expired - Fee Related
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109823545A (en) * | 2019-03-27 | 2019-05-31 | 河南机电职业学院 | A kind of injection recoil force eliminating device and removing method for hybrid power unmanned plane |
CN109823545B (en) * | 2019-03-27 | 2024-02-09 | 河南机电职业学院 | Injection recoil eliminating method for hybrid unmanned aerial vehicle |
CN110339515A (en) * | 2019-08-02 | 2019-10-18 | 张廷建 | Pneumatic power flight robot fire-fighting system and the method put out a fire using the system |
CN110339515B (en) * | 2019-08-02 | 2024-05-24 | 明光安鲁科技有限公司 | Pneumatic flying robot fire-fighting system and fire-extinguishing method using same |
CN112370689A (en) * | 2019-10-28 | 2021-02-19 | 周丽娟 | Novel communication wire and cable fire extinguishing unmanned aerial vehicle |
CN112370690A (en) * | 2019-10-28 | 2021-02-19 | 周丽娟 | Novel communication wire and cable fire extinguishing unmanned aerial vehicle |
CN112370690B (en) * | 2019-10-28 | 2021-07-30 | 苏州维斯勒姆智能科技有限公司 | Communication wire and cable fire extinguishing unmanned aerial vehicle |
CN112370689B (en) * | 2019-10-28 | 2021-08-03 | 苏州维斯勒姆智能科技有限公司 | Communication wire and cable fire extinguishing unmanned aerial vehicle |
CN111529993A (en) * | 2020-04-29 | 2020-08-14 | 中国民用航空飞行学院 | Be applied to unmanned aerial vehicle's suspension extinguishing device |
CN111529993B (en) * | 2020-04-29 | 2021-06-11 | 中国民用航空飞行学院 | Be applied to unmanned aerial vehicle's suspension extinguishing device |
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Granted publication date: 20190108 |