CN208339950U - A kind of high building fire fighting aviation mechanism - Google Patents

A kind of high building fire fighting aviation mechanism Download PDF

Info

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
Authority
CN
China
Prior art keywords
water
main body
fire fighting
platform
building fire
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.)
Expired - Fee Related
Application number
CN201820148637.9U
Other languages
Chinese (zh)
Inventor
王颜琦
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CN201820148637.9U priority Critical patent/CN208339950U/en
Application granted granted Critical
Publication of CN208339950U publication Critical patent/CN208339950U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • 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

A kind of high building fire fighting aviation mechanism
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.
CN201820148637.9U 2018-01-29 2018-01-29 A kind of high building fire fighting aviation mechanism Expired - Fee Related CN208339950U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201820148637.9U CN208339950U (en) 2018-01-29 2018-01-29 A kind of high building fire fighting aviation mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201820148637.9U CN208339950U (en) 2018-01-29 2018-01-29 A kind of high building fire fighting aviation mechanism

Publications (1)

Publication Number Publication Date
CN208339950U true CN208339950U (en) 2019-01-08

Family

ID=64874876

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201820148637.9U Expired - Fee Related CN208339950U (en) 2018-01-29 2018-01-29 A kind of high building fire fighting aviation mechanism

Country Status (1)

Country Link
CN (1) CN208339950U (en)

Cited By (4)

* Cited by examiner, † Cited by third party
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
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

Cited By (10)

* Cited by examiner, † Cited by third party
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

Similar Documents

Publication Publication Date Title
CN208339950U (en) A kind of high building fire fighting aviation mechanism
EP3587265B1 (en) Air-transportable device for projecting pressurised liquid
US20180118341A1 (en) Unmanned flying spray system
CN207125992U (en) A kind of unmanned plane high-altitude fire extinguishing system
CN107115604A (en) A kind of fire-fighting and rescue system
CN102343978A (en) Fine water mist fire-fighting helicopter
CN106828901A (en) Towing power lead formula multiaxis rotor wing unmanned aerial vehicle extinguishing device and extinguishing method
CN109162431A (en) A kind of high building wall spray robot
CN109436327B (en) Automatic unmanned aerial vehicle puts out a fire
WO2020052106A1 (en) Compact long-endurance crop protecting unmanned aerial vehicle
CN105059546A (en) Electric unmanned helicopter provided with water and electricity supply pipeline and used for high-rise and mountain forest extinguishment
CN111361740A (en) Water flow supercharged cleaning system and method based on tethered unmanned aerial vehicle platform
CN102179015B (en) Fire extinguishing device for high-rise building
CN112807591A (en) Intelligent fire extinguishing device for building
CN211167419U (en) A novel many rotor unmanned aerial vehicle for putting out a fire
CN204582340U (en) High-level crane fire-fighting system
CN201678043U (en) Hydraulic helicopter
CN209422820U (en) A kind of high-altitude fire extinguishing system based on unmanned plane
CN103405867A (en) Overhead fixed-point continuous water spraying device based on hot air balloon
CN107126651A (en) A kind of fire-fighting system
CN110915785A (en) Fire-fighting hornet nest processing device and method applicable to multiple scenes
CN106765812B (en) Humidification system capable of sterilizing and disinfecting
CN208217006U (en) A kind of shatter-resistant plant protection drone
CN107115605A (en) A kind of fire-fighting system and its fire-fighting mode
CN108557067A (en) A kind of nothing is risen and fallen posture small drone

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: 20190108