CN205044962U - Multi -functional fire control aircraft - Google Patents
Multi -functional fire control aircraft Download PDFInfo
- Publication number
- CN205044962U CN205044962U CN201520665809.6U CN201520665809U CN205044962U CN 205044962 U CN205044962 U CN 205044962U CN 201520665809 U CN201520665809 U CN 201520665809U CN 205044962 U CN205044962 U CN 205044962U
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- power supply
- cable
- connection pipe
- fire
- aircraft
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Abstract
The utility model relates to a multi -functional fire control aircraft, including unmanned vehicles and ground power supply unit, still include landing leg, extinguishing device, cable and camera, the unmanned vehicles bottom sets up the landing leg, and extinguishing device hangs on the landing leg, and ground power supply unit passes through cable and unmanned vehicles electric connection, and the camera is installed on the landing leg. The utility model has the advantages of 1, ground power supply unit passes through cable and unmanned vehicles electric connection, and the flight scheme of carrying on the battery with current unmanned vehicles is compared, uses wired ground power supply unit power supply plan, enables the flight time greatly increased of aircraft, increases the payload of aircraft. 2, fire extinguishing performance is superior, and fire extinguishing efficiency is high, extinguishing device be dry powder extinguishing device flow greatly, long firing range, effectively stamp out various remote conflagration.
Description
Technical field
The utility model relates to a kind of fire extinguisher, particularly relates to a kind of multifunctional fire-fighting aircraft.
Background technology
Flying instrument has maneuverability, cheap advantage.Use aircraft as the carrier of fire-fighting equipment, can solve high-rise fire fighting difficulty, not easily observe a difficult problem for the condition of a fire, fire fighting efficiency is high, eliminates the potential safety hazard of firefighter.
But, there is following problem at present: existing product adopts lithium cell etc. to power to aircraft, because aircraft energy consumption is comparatively large so power consumption quickly, causes the cruise duration of aircraft short, although carry high capacity cell can extend the flight time, the capacity weight of aircraft is caused to reduce; Secondly, adopt communicating wireless signals between the watch-dog of lift-launch and ground, the image quality of transmission is poor.
Utility model content
Technical problem to be solved in the utility model is: provide a kind of multifunctional fire-fighting aircraft, solves high-rise high-rise fire fighting difficulty, not easily observes the problem of the condition of a fire, overcome the deficiency that cruise duration is short, capacity weight is low simultaneously.
The technical scheme that the problem that the utility model is the above-mentioned proposition of solution adopts is:
A kind of multifunctional fire-fighting aircraft, comprise unmanned vehicle 1 and floor power supply device 2, also comprise supporting leg 3, fire extinguisher plant 4, cable 5 and camera 6, supporting leg 3 is set bottom unmanned vehicle 1, fire extinguisher plant 4 is suspended on supporting leg 3, floor power supply device 2 is electrically connected by cable 5 and unmanned vehicle 1, and camera 6 is arranged on supporting leg 3.
Described camera 6 is high definition line camera.
Bottom described supporting leg 3, fast window breaker 33 is set, realizes the object of broken window fast.
Described floor power supply device 2 comprises electric power system 7 and wire spool 8, and cable 5 is wrapped on wire spool 8.
Described wire spool 8 comprises rectangular frame 23, control cage 24, crosswise joint roller 25, upright controling roller 26, reel 27, rotating shaft 28, rocking bar 29 and handle 30, rectangular frame 23 front end arranges control cage 24, control cage 24 is provided with crosswise joint roller 25 and upright controling roller 26, reel 27 center arranges rotating shaft 28, rotating shaft 28 one end is fixedly connected with rocking bar 29 through rectangular frame 23, rocking bar 29 other end mounting handle 30.
Described rectangular frame 23 front bottom end arranges support 31, and rectangular frame 23 arranges bandage 32 bottom rear end.
Described fire extinguisher plant 4 comprises dry powder can 9, liquid carbon dioxide bottle 10, threeway 11, self-priming blending box 12, connection pipe A13, connection pipe B14, connection pipe C15 and jet pipe 16, dry powder can 9 is connected with the first arm of threeway 11 by connection pipe A13, self-priming blending box 12 is connected with the second arm of threeway 11 by connection pipe B14, connection pipe C15 one end is communicated with dry powder can 9, the connection pipe C15 other end is communicated with self-priming blending box 12, liquid carbon dioxide bottle 10 is connected with the supervisor of threeway 11, and jet pipe 16 is communicated with self-priming blending box 12.
Described connection pipe A13 arranges limiting valve 17.
Described connection pipe B14 arranges electrically-controlled valve 18.
Described cable 5 comprises conductor 19, insulating barrier 20, restrictive coating 21 and steel rope 22, sets gradually insulating barrier 20, restrictive coating 21, arrange steel rope 22 in restrictive coating 21 outside conductor 19.
Principle of work of the present utility model: bottom unmanned vehicle, supporting leg is set, fire extinguisher plant is suspended on supporting leg, floor power supply device is electrically connected by cable and unmanned vehicle, compared with the flight scenario that existing unmanned vehicle is battery-mounted, uses wired floor power supply device power supply plan; Camera is arranged on supporting leg.
The beneficial effects of the utility model are: 1, floor power supply device is electrically connected by cable and unmanned vehicle, compared with the flight scenario that existing unmanned vehicle is battery-mounted, use wired floor power supply device power supply plan, the flight time of aircraft can be made greatly to increase, increase the capacity weight of aircraft.2, extinguishing property is superior, and fire-fighting efficiency is high, and fire extinguisher plant is that dry powder extinguishing installation flow is large, far firing range, effectively puts out various remote fire.3, aircraft is provided with standby lithium pond group, can standby electricity be connected when cable surprisingly ruptures, avoid aircraft to drop from height in the air and hurt sb.'s feelings and cause device damage.4, replace aerial ladder, elevator operation, water-band lift-off can be carried and put out a fire, mobility strong, to be swift in response, reduce the personal casualty in the middle of fire fighting and rescue fight as far as possible, ensure firefighters life security.5, carry escaping rope, escaping rope, Rope ladder for escaping can be thrown to the room that catches fire, set up tunnel escape.6, camera is high definition line camera.7, cable adopts flame retardant high-strength cable, and flame resistance is strong, and intensity is high.8, bottom supporting leg, fast window breaker is set, realizes the object of broken window fast.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model;
Fig. 2 is the schematic cross-section of cable in Fig. 1.
Wherein, 1-unmanned vehicle, 2-floor power supply device, 3-supporting leg, 4-fire extinguisher plant, 5-cable, 6-camera, 7-electric power system, 8-wire spool, 9-dry powder can, 10-liquid carbon dioxide bottle, 11-threeway, the self-priming blending box of 12-, 13-connection pipe A, 14-connection pipe B, 15-connection pipe C, 16-jet pipe, 17-limiting valve, 18-electrically-controlled valve, 19-conductor, 20-insulating barrier, 21-restrictive coating, 22-steel rope, 23-rectangular frame, 24-control cage, 25-crosswise joint roller, 26-upright controling roller, 27-reel, 28-rotating shaft, 29-rocking bar, 30-handle, 31-support, 32-bandage, 33-fast window breaker.
Detailed description of the invention
Embodiment of the present utility model is further illustrated below in conjunction with accompanying drawing.
With reference to Fig. 1-2, a kind of multifunctional fire-fighting aircraft described in this detailed description of the invention, comprise unmanned vehicle 1 and floor power supply device 2, also comprise supporting leg 3, fire extinguisher plant 4, cable 5 and camera 6, supporting leg 3 is set bottom unmanned vehicle 1, fire extinguisher plant 4 is suspended on supporting leg 3, and floor power supply device 2 is electrically connected by cable 5 and unmanned vehicle 1, and camera 6 is arranged on supporting leg 3.
Described unmanned vehicle 1 is many rotor unmanned aircrafts.
Described camera 6 is high definition line camera.
Bottom described supporting leg 3, fast window breaker 33 is set, realizes the object of broken window fast.
Described floor power supply device 2 comprises electric power system 7 and wire spool 8, and cable 5 is wrapped on wire spool 8.
Described wire spool 8 comprises rectangular frame 23, control cage 24, crosswise joint roller 25, upright controling roller 26, reel 27, rotating shaft 28, rocking bar 29 and handle 30, rectangular frame 23 front end arranges control cage 24, control cage 24 is provided with crosswise joint roller 25 and upright controling roller 26, reel 27 center arranges rotating shaft 28, rotating shaft 28 one end is fixedly connected with rocking bar 29 through rectangular frame 23, rocking bar 29 other end mounting handle 30.
Described rectangular frame 23 front bottom end arranges support 31, and rectangular frame 23 arranges bandage 32 bottom rear end.
Described fire extinguisher plant 4 comprises dry powder can 9, liquid carbon dioxide bottle 10, threeway 11, self-priming blending box 12, connection pipe A13, connection pipe B14, connection pipe C15 and jet pipe 16, dry powder can 9 is connected with the first arm of threeway 11 by connection pipe A13, self-priming blending box 12 is connected with the second arm of threeway 11 by connection pipe B14, connection pipe C15 one end is communicated with dry powder can 9, the connection pipe C15 other end is communicated with self-priming blending box 12, liquid carbon dioxide bottle 10 is connected with the supervisor of threeway 11, and jet pipe 16 is communicated with self-priming blending box 12.
Described connection pipe A13 arranges limiting valve 17.
Described connection pipe B14 arranges electrically-controlled valve 18.
Described cable 5 comprises conductor 19, insulating barrier 20, restrictive coating 21 and steel rope 22, sets gradually insulating barrier 20, restrictive coating 21, arrange steel rope 22 in restrictive coating 21 outside conductor 19.
The principle of work of this detailed description of the invention: bottom unmanned vehicle, supporting leg is set, fire extinguisher plant is suspended on supporting leg, floor power supply device is electrically connected by cable and unmanned vehicle, compared with the flight scenario that existing unmanned vehicle is battery-mounted, use wired floor power supply device power supply plan; Camera is arranged on supporting leg.
The beneficial effect of this detailed description of the invention is: 1, floor power supply device is electrically connected by cable and unmanned vehicle, compared with the flight scenario that existing unmanned vehicle is battery-mounted, use wired floor power supply device power supply plan, the flight time of aircraft can be made greatly to increase, increase the capacity weight of aircraft.2, extinguishing property is superior, and fire-fighting efficiency is high, and fire extinguisher plant is that dry powder extinguishing installation flow is large, far firing range, effectively puts out various remote fire.3, aircraft is provided with standby lithium pond group, can standby electricity be connected when cable surprisingly ruptures, avoid aircraft to drop from height in the air and hurt sb.'s feelings and cause device damage.4, replace aerial ladder, elevator operation, water-band lift-off can be carried and put out a fire, mobility strong, to be swift in response, reduce the personal casualty in the middle of fire fighting and rescue fight as far as possible, ensure firefighters life security.5, carry escaping rope, escaping rope, Rope ladder for escaping can be thrown to the room that catches fire, set up tunnel escape.6, camera is high definition line camera.7, cable adopts flame retardant high-strength cable, and flame resistance is strong, and intensity is high.8, bottom supporting leg, fast window breaker is set, realizes the object of broken window fast.
Specific embodiment of the utility model does not form restriction of the present utility model, and every employing analog structure of the present utility model and change, all in protection domain of the present utility model.
Claims (5)
1. a multifunctional fire-fighting aircraft, comprise unmanned vehicle (1) and floor power supply device (2), it is characterized in that: also comprise supporting leg (3), fire extinguisher plant (4), cable (5) and camera (6), unmanned vehicle (1) bottom arranges supporting leg (3), fire extinguisher plant (4) is suspended on supporting leg (3), floor power supply device (2) is electrically connected by cable (5) and unmanned vehicle (1), and camera (6) is arranged on supporting leg (3).
2. a kind of multifunctional fire-fighting aircraft as claimed in claim 1, is characterized in that: described floor power supply device (2) comprises electric power system (7) and wire spool (8), and cable (5) is wrapped on wire spool (8).
3. a kind of multifunctional fire-fighting aircraft as claimed in claim 2, it is characterized in that: described wire spool (8) comprises rectangular frame (23), control cage (24), crosswise joint roller (25), upright controling roller (26), reel (27), rotating shaft (28), rocking bar (29) and handle (30), rectangular frame (23) front end arranges control cage (24), control cage (24) is provided with crosswise joint roller (25) and upright controling roller (26), reel (27) center arranges rotating shaft (28), rotating shaft (28) one end is fixedly connected with rocking bar (29) through rectangular frame (23), rocking bar (29) other end mounting handle (30).
4. a kind of multifunctional fire-fighting aircraft as claimed in claim 1, it is characterized in that: described fire extinguisher plant (4) comprises dry powder can (9), liquid carbon dioxide bottle (10), threeway (11), self-priming blending box (12), connection pipe A(13), connection pipe B(14), connection pipe C(15) and jet pipe (16), dry powder can (9) is by connection pipe A(13) be connected with the first arm of threeway (11), self-priming blending box (12) is by connection pipe B(14) be connected with the second arm of threeway (11), connection pipe C(15) one end connection dry powder can (9), connection pipe C(15) other end is communicated with self-priming blending box (12), liquid carbon dioxide bottle (10) is connected with the supervisor of threeway (11), jet pipe (16) is communicated with self-priming blending box (12).
5. a kind of multifunctional fire-fighting aircraft as claimed in claim 1, it is characterized in that: described cable (5) comprises conductor (19), insulating barrier (20), restrictive coating (21) and steel rope (22), conductor (19) outside sets gradually insulating barrier (20), restrictive coating (21), arranges steel rope (22) in restrictive coating (21).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201520665809.6U CN205044962U (en) | 2015-08-31 | 2015-08-31 | Multi -functional fire control aircraft |
Applications Claiming Priority (1)
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CN201520665809.6U CN205044962U (en) | 2015-08-31 | 2015-08-31 | Multi -functional fire control aircraft |
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CN205044962U true CN205044962U (en) | 2016-02-24 |
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CN201520665809.6U Expired - Fee Related CN205044962U (en) | 2015-08-31 | 2015-08-31 | Multi -functional fire control aircraft |
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Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105816981A (en) * | 2016-03-29 | 2016-08-03 | 国网山东省电力公司烟台供电公司 | Fire extinguishing apparatus for high-altitude electric power equipment |
CN106075765A (en) * | 2016-08-05 | 2016-11-09 | 杨勇 | A kind of hydrodynamic force fire-fighting aircraft |
CN106114834A (en) * | 2016-06-28 | 2016-11-16 | 安徽扫宝智能科技有限公司 | A kind of aerial electric circuit fire-fighting and rescue six axle aircraft |
CN106114859A (en) * | 2016-06-28 | 2016-11-16 | 安徽扫宝智能科技有限公司 | A kind of aerial electric electrical network fire extinguishing job that requires special skills unmanned plane |
TWI573732B (en) * | 2016-04-28 | 2017-03-11 | xin-jia Lin | An unmanned vehicle with a remote powered project |
CN108404318A (en) * | 2018-05-23 | 2018-08-17 | 深圳飞凡空中机器人有限公司 | One kind being tethered at power supply dry powder fire-fighting unmanned plane |
CN109204856A (en) * | 2017-07-03 | 2019-01-15 | 深圳市道通智能航空技术有限公司 | Holder and unmanned plane with this holder |
CN112960114A (en) * | 2021-02-04 | 2021-06-15 | 国家能源(山东)工程技术有限公司 | Fire control unmanned aerial vehicle |
-
2015
- 2015-08-31 CN CN201520665809.6U patent/CN205044962U/en not_active Expired - Fee Related
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105816981A (en) * | 2016-03-29 | 2016-08-03 | 国网山东省电力公司烟台供电公司 | Fire extinguishing apparatus for high-altitude electric power equipment |
TWI573732B (en) * | 2016-04-28 | 2017-03-11 | xin-jia Lin | An unmanned vehicle with a remote powered project |
CN106114834A (en) * | 2016-06-28 | 2016-11-16 | 安徽扫宝智能科技有限公司 | A kind of aerial electric circuit fire-fighting and rescue six axle aircraft |
CN106114859A (en) * | 2016-06-28 | 2016-11-16 | 安徽扫宝智能科技有限公司 | A kind of aerial electric electrical network fire extinguishing job that requires special skills unmanned plane |
CN106114859B (en) * | 2016-06-28 | 2018-04-27 | 林伟滨 | A kind of aerial electric power grid fire extinguishing job that requires special skills unmanned plane |
CN106075765A (en) * | 2016-08-05 | 2016-11-09 | 杨勇 | A kind of hydrodynamic force fire-fighting aircraft |
CN109204856A (en) * | 2017-07-03 | 2019-01-15 | 深圳市道通智能航空技术有限公司 | Holder and unmanned plane with this holder |
CN108404318A (en) * | 2018-05-23 | 2018-08-17 | 深圳飞凡空中机器人有限公司 | One kind being tethered at power supply dry powder fire-fighting unmanned plane |
CN112960114A (en) * | 2021-02-04 | 2021-06-15 | 国家能源(山东)工程技术有限公司 | Fire control unmanned aerial vehicle |
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Legal Events
Date | Code | Title | Description |
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C14 | Grant of patent or utility model | ||
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: 20160224 Termination date: 20160831 |