CN204864620U - Unmanned aerial vehicle carries extinguishing device - Google Patents
Unmanned aerial vehicle carries extinguishing device Download PDFInfo
- Publication number
- CN204864620U CN204864620U CN201520500569.4U CN201520500569U CN204864620U CN 204864620 U CN204864620 U CN 204864620U CN 201520500569 U CN201520500569 U CN 201520500569U CN 204864620 U CN204864620 U CN 204864620U
- Authority
- CN
- China
- Prior art keywords
- gun barrel
- extinguishing device
- bogey
- uav system
- carrier
- 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.)
- Active
Links
Landscapes
- Toys (AREA)
Abstract
The utility model discloses an unmanned aerial vehicle carries extinguishing device, including the carrier and be used for the broken window bullet of transmission first barrel and be used for launching the second barrel of fire extinguishing bomb, first barrel and the equal fixed mounting of second barrel are on the carrier. The utility model discloses be equipped with the two barrel simultaneously, loaded brokenly window bullet and fire extinguishing bomb, can realize brokenly two kinds of functions of window and outfire simultaneously.
Description
Technical field
The utility model relates to extinguishing device, refers to a kind of UAV system extinguishing device especially.
Background technology
Along with the development of modern society, the fire-fighting consciousness of people is also in continuous enhancing, and fire-fighting equipment is also at development thereupon.But modern building is built more and more higher, traditional fire-fighting equipment cannot provide fire-fighting guarantee already.Based on this, see the Chinese invention patent application Publication Specification that publication number is CN104027909A, which provide the police unmanned plane of a kind of high building, comprise earth station and earth station's two parts, described unmanned plane comprises unmanned plane main body, three axle The Cloud Terraces, fire extinguisher bomb launching tube and takes aim at tool, and described unmanned plane main body is built with having GPS positioner and radar avoiding device.Earth station can control the direction of three axle The Cloud Terraces, and make to take aim at tool and aim at burning things which may cause a fire disaster, fire extinguisher bomb launching tube launches fire extinguisher bomb afterwards, puts out burning things which may cause a fire disaster.The positional information of unmanned plane can be passed to earth station by GPS positioner, is shared with other multiple unmanned planes, jointly puts out burning things which may cause a fire disaster.
When this mode solves to a certain extent thus solution high-rise can be helped to catch fire, aerial ladder of fire truck insufficient height, be difficult to the problem of fire extinguishing in time, but it still has following problem: general when skyscraper catches fire, its curtain wall is comparatively abundant, is difficult to burn for the moment, and Extinguishing bomb is generally difficult to realize real broken window, because the structure of fire extinguisher bomb is hung fire after transmitting, if front end is too hard, then cause the effect cannot reaching effectively blast.And said method needs an other unmanned plane to carry out transmitting fire extinguisher bomb after broken window, and follow-up unmanned plane is differed the precision reaching surely and accurately launched fire extinguisher bomb by curtain wall broken hole.
Utility model content
The utility model proposes a kind of UAV system extinguishing device, utilize a frame unmanned plane to solve brokenly the problem of window and fire extinguishing simultaneously.
The technical solution of the utility model is achieved in that a kind of UAV system extinguishing device, comprises carrier, also comprises launching brokenly the first gun barrel of window bullet and the second gun barrel in order to launch fire extinguisher bomb, and the first gun barrel and the second gun barrel are fixed on carrier.
Further, carrier is three axle The Cloud Terraces or two axle The Cloud Terraces.
Further, the first gun barrel and the second gun barrel all adopt compressed air or gunpowder to launch.
Further, carrier is provided with the bogey installing the first gun barrel and the second gun barrel.Further, be provided with magazine in bogey, magazine is built with broken window bullet and fire extinguisher bomb.Bogey is provided with laser aiming instrument and camera, laser aiming instrument, camera, the first gun barrel and the second gun barrel are arranged on the same side of bogey.Further, bogey is also provided with the hotness instrument for finding out burning things which may cause a fire disaster.Be provided with bomb droping gear bottom bogey, bomb droping gear is the carry device by the dodge gate of switch control rule or assembling fire extinguisher bomb.
Further, carrier can be directly fixedly connected with unmanned plane or be fixedly connected with unmanned plane by fixture.Further, fixture comprises installing rack, elastic component and fixed mount, and installing rack is fixed on unmanned plane, and is connected with fixed mount by elastic component, and fixed mount is fixedly connected with carrier.
The beneficial effects of the utility model are: the utility model proposes a kind of extinguishing device based on unmanned plane, fire extinguishing can be helped when aerial ladder insufficient height, the utility model is provided with two kinds of gun barrels, be filled with brokenly window bullet and fire extinguisher bomb respectively, window and fire extinguishing can be broken, without using other unmanned plane simultaneously.
Accompanying drawing explanation
In order to be illustrated more clearly in the utility model embodiment or technical scheme of the prior art, be briefly described to the accompanying drawing used required in embodiment or description of the prior art below, apparently, accompanying drawing in the following describes is only embodiments more of the present utility model, for those of ordinary skill in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to these accompanying drawings.
Fig. 1 is the structural representation of the utility model first embodiment;
Fig. 2 is the structural representation of the utility model second embodiment;
Fig. 3 is the structural representation of the bogey of the utility model the 3rd embodiment;
Fig. 4 is the structural representation of the bogey of the utility model the 4th embodiment;
Fig. 5 is the sectional view of the second gun barrel of the present utility model.
In figure, 1-first cursor; 2-second cursor; 3-first motor; 4-second motor; 5-the 3rd motor; 6-turning cylinder; 7-laser aiming instrument; 8-camera; 9-first gun barrel; 10-second gun barrel; 11-bogey; 12-installing rack; 13-elastic component; 14-fixed mount; 15-circuit board; 16-magazine; 17-fire extinguisher bomb; 18-striker; 19-percussion lock; 20-elastomeric element; 21-dodge gate; 22-switch; 23-carry device.
Detailed description of the invention
Below in conjunction with the accompanying drawing in the utility model embodiment, be clearly and completely described the technical scheme in the utility model embodiment, obviously, described embodiment is only the utility model part embodiment, instead of whole embodiments.Based on the embodiment in the utility model, those of ordinary skill in the art are not making the every other embodiment obtained under creative work prerequisite, all belong to the scope of the utility model protection.
Fig. 1 is an embodiment of a kind of UAV system extinguishing device of the utility model, UAV system extinguishing device comprises carrier and in order to the first gun barrel 9 of launching brokenly window bullet and the second gun barrel 10 in order to launch fire extinguisher bomb 17, first gun barrel 9 also can load fire extinguisher bomb 17, second gun barrel 10 can load brokenly window bullet, and the number of the first gun barrel 9 and the second gun barrel 10 is at least one; Carrier is fixed with bogey 11, the first gun barrel 9 and the second gun barrel 10 are all fixedly mounted on the side of bogey 11.Bogey 11 inner bottom part is provided with magazine 16 and fire extinguisher bomb 17 container cavity, and magazine 16 is built with broken window bullet and fire extinguisher bomb 17, and bogey 11 lower end also can be provided with slot, in order to throw fire extinguisher bomb 17.Also carry device carry fire extinguisher bomb 17 can be adopted to throw in bogey 11 lower end, such structure change still falls within protection domain of the present utility model.
In the present embodiment, the first gun barrel 9 and the second gun barrel 10 difference built-in broken window bullet and fire extinguisher bomb 17 in advance, and adopt compressed air to launch.Namely the first gun barrel 9 and the second gun barrel 10 are air bubble, and air bubble adopts prior art, and therefore not to repeat here.
Carrier is three axle The Cloud Terraces or two axle The Cloud Terraces, in the present embodiment, carrier is three axle The Cloud Terraces, comprise the first cursor 1 and the second cursor 2, first cursor 1 comprises two support arms be mutually vertically fixed on together, presents L shape, one of them support arm is fixed with the first motor 3, first motor 3 is fixedly connected with fixed mount 14 lower end, and another support arm and the second cursor 2 link together.
Second cursor 2 is U-shaped structure, the bottom of U-shaped structure is provided with the second motor 4, and the top of U-shaped structure is provided with the 3rd motor 5 and turning cylinder the 6, three motor 5 and turning cylinder 6 and links together, second cursor 2 is driven by the second motor 4, and turning cylinder 6 is driven by the 3rd motor 5; Turning cylinder 6 is fixed with bogey 11.
First motor 3, second motor 4 and the 3rd motor 5 are brushless electric machine, the connected mode of the first motor 3, second motor 4 and the 3rd motor 5 and the first cursor 1 and the second cursor 2 can adopt and directly be connected, rotational angle is more accurate, and rotational response is also more sensitive.In other embodiments, also can adopt by transmission mechanism as worm-and-wheel gear connects.
Bogey 11 is provided with laser aiming instrument 7 and camera 8, laser aiming instrument 7, camera 8, first gun barrel 9 and the second gun barrel 10 are arranged on the same side of bogey 11.In addition bogey 11 is also provided with the hotness instrument for finding out burning things which may cause a fire disaster.
In this embodiment, carrier is directly fixed on unmanned plane.
Fig. 2 is another embodiment of the present utility model, and in this embodiment, carrier is fixedly connected with unmanned plane by fixture.Fixture comprises installing rack 12, elastic component 13 and fixed mount 14, installing rack 12 can be made into metallic plate, be screwed in lower end or other positions of unmanned plane, installing rack 12 is connected with fixed mount 14 by multiple elastic component 13, the number of elastic component 13 can be four, and concrete number does not limit; Fixed mount 14 can be made into various shape, and one end of fixed mount 14 is fixedly connected with elastic component 13, and the other end is fixedly connected with carrier.
Be provided with magazine 16 in bogey 11, magazine 16 is built with broken window bullet and fire extinguisher bomb 17.In the present embodiment, the first gun barrel 9 and the second gun barrel 10 all adopt gunpowder to launch, and compressed-air actuated mode also can be adopted to launch, and such change still falls within protection domain of the present utility model.And in bogey 11, be provided with two magazines 16, be connected with the first gun barrel 9 and the second gun barrel 10 respectively, in two magazines 16, be respectively equipped with brokenly window bullet and fire extinguisher bomb 17.In other embodiments, also a magazine 16 only can be set, in magazine 16, establish fire extinguisher bomb 17, and be connected with the second gun barrel 10, in the first gun barrel 9, preset broken window bullet.
Bogey 11 is provided with laser aiming instrument 7 and camera 8, laser aiming instrument 7, camera 8, first gun barrel 9 and the second gun barrel 10 are arranged on the same side of bogey 11.In addition bogey 11 is also provided with the hotness instrument for finding out burning things which may cause a fire disaster, and by controller connection carrier, to control the transmit direction of each gun barrel, ensures that the utility model UAV system extinguishing device can directly control burning things which may cause a fire disaster.
In the present embodiment, the first cursor 1, in bending the circular arc turned to, so, has better mechanical property, ensure that the first cursor 1 intensity.First cursor 1 can be also linear pattern cursor or circular arc cursor, and the utility model is not construed as limiting this, and the first cursor 1 of other shapes still falls within protection domain of the present utility model.
Fig. 3 is the structural representation of the bogey 11 of the 3rd embodiment of the present utility model, as shown in Figure 3, in this embodiment, the structure of bogey 11 is improved, the bottom outside of bogey 11 is fixed with carry device 23, and carry device 23 is provided with fire extinguisher bomb 17, except the second gun barrel 10, bogey 11 launches fire extinguisher bomb 17 by carry device 23, can launch two fire extinguisher bombs simultaneously.
Fig. 4 is the structural representation of the bogey 11 of the 3rd embodiment of the present utility model, as shown in Figure 4, in this embodiment, the structure of bogey 11 is improved, bogey 11 outside is provided with the second gun barrel 10, inside is provided with circuit board 15 and magazine 16, fire extinguisher bomb 17 is filled with in magazine 16, in addition, be provided with the switch 22 of dodge gate 21 and control dodge gate 21 bottom bogey 11, adopt this structure, except the second gun barrel 10, bogey 11 also launches fire extinguisher bomb 17 by the dodge gate 21 of bottom, and fire-fighting efficiency is higher.
Fig. 5 is the sectional view of the second gun barrel, as shown in Figure 5, what the second gun barrel 10 connected has percussion lock 19, striker 18 is provided with in percussion lock 19, percussion lock 19 and striker 18, for launching fire extinguisher bomb 17, are provided with circuit board 15 and magazine 16, are filled with fire extinguisher bomb 17 in magazine 16 inside bogey 11, be provided with elastomeric element 20 bottom magazine 16, elastomeric element 20 can fire extinguisher bomb 17 bullet in the second gun barrel 10.
The utility model proposes a kind of extinguishing device based on unmanned plane, can help fire extinguishing when aerial ladder insufficient height, the utility model is provided with two kinds of gun barrels, is filled with brokenly window bullet and fire extinguisher bomb respectively, window and fire extinguishing can be broken, without using other unmanned plane simultaneously.
These are only preferred embodiment of the present utility model, not in order to limit the utility model, all within spirit of the present utility model and principle, any amendment done, equivalent replacement, improvement etc., all should be included within protection domain of the present utility model.
Claims (10)
1. a UAV system extinguishing device, comprises carrier, it is characterized in that: also comprise launching brokenly the first gun barrel of window bullet and the second gun barrel in order to launch fire extinguisher bomb, and described first gun barrel and described second gun barrel are fixed on the carrier.
2. a kind of UAV system extinguishing device according to claim 1, is characterized in that: described carrier is three axle The Cloud Terraces or two axle The Cloud Terraces.
3. a kind of UAV system extinguishing device according to claim 1, is characterized in that: described first gun barrel and the second gun barrel all adopt compressed air or gunpowder to launch.
4. a kind of UAV system extinguishing device according to claim 1, is characterized in that: described carrier is provided with to install the bogey of described first gun barrel and described second gun barrel.
5. a kind of UAV system extinguishing device according to claim 4, is characterized in that: be provided with magazine in described bogey, and described magazine is built with broken window bullet and fire extinguisher bomb.
6. a kind of UAV system extinguishing device according to claim 4, it is characterized in that: described bogey is provided with laser aiming instrument and camera, described laser aiming instrument, camera, the first gun barrel and the second gun barrel are arranged on the same side of bogey.
7. a kind of UAV system extinguishing device according to claim 6, is characterized in that: described bogey is also provided with the hotness instrument for finding out burning things which may cause a fire disaster.
8. a kind of UAV system extinguishing device according to any one of claim 4-7, is characterized in that: be provided with bomb droping gear bottom described bogey, and described bomb droping gear is the carry device by the dodge gate of switch control rule or assembling fire extinguisher bomb.
9. a kind of UAV system extinguishing device according to claim 1, is characterized in that: described carrier can be directly fixedly connected with unmanned plane or be fixedly connected with unmanned plane by fixture.
10. a kind of UAV system extinguishing device according to claim 9, it is characterized in that: described fixture comprises installing rack, elastic component and fixed mount, described installing rack is fixed on unmanned plane, and is connected with fixed mount by elastic component, and described fixed mount is fixedly connected with carrier.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201520500569.4U CN204864620U (en) | 2015-07-10 | 2015-07-10 | Unmanned aerial vehicle carries extinguishing device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201520500569.4U CN204864620U (en) | 2015-07-10 | 2015-07-10 | Unmanned aerial vehicle carries extinguishing device |
Publications (1)
Publication Number | Publication Date |
---|---|
CN204864620U true CN204864620U (en) | 2015-12-16 |
Family
ID=54809059
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201520500569.4U Active CN204864620U (en) | 2015-07-10 | 2015-07-10 | Unmanned aerial vehicle carries extinguishing device |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN204864620U (en) |
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106871740A (en) * | 2017-03-30 | 2017-06-20 | 西安天鹰防务科技有限公司 | The application of barrel assemblies, shell carry frame and shell carry frame on unmanned plane |
CN107261376A (en) * | 2017-08-07 | 2017-10-20 | 沈阳金丰春航空科技有限公司 | Unmanned plane and fire-extinguishing |
CN107456683A (en) * | 2017-08-14 | 2017-12-12 | 苏州凸现信息科技有限公司 | A kind of skyscraper fire fighting device and its method of work based on unmanned plane |
CN107670201A (en) * | 2017-08-31 | 2018-02-09 | 上海机电工程研究所 | UAV system type fire extinguishing system |
CN108168371A (en) * | 2017-12-27 | 2018-06-15 | 深圳城际快机科技有限公司 | A kind of more bullet kinds of unmanned plane emit sighting device and system |
CN108313279A (en) * | 2018-04-09 | 2018-07-24 | 重庆国飞通用航空设备制造有限公司 | A kind of special fire extinguishing multi-rotor unmanned aerial vehicle system of fire-fighting |
CN108454839A (en) * | 2018-04-09 | 2018-08-28 | 重庆国飞通用航空设备制造有限公司 | A kind of efficient emergency broken window multi-rotor unmanned aerial vehicle system |
CN109464766A (en) * | 2018-09-14 | 2019-03-15 | 广州市华科尔科技股份有限公司 | A kind of fire-fighting method of fire-fighting unmanned plane |
CN109733876A (en) * | 2019-01-04 | 2019-05-10 | 京东方科技集团股份有限公司 | A kind of fetching device and pick and place method |
CN110270020A (en) * | 2019-07-08 | 2019-09-24 | 西安航天化学动力有限公司 | A kind of Recoilless window breaker of UAV system |
WO2020043223A1 (en) * | 2018-08-27 | 2020-03-05 | MÁTL, Roman | Mobile fire extinguishing equipment |
CN113908469A (en) * | 2021-10-29 | 2022-01-11 | 亿航智能设备(广州)有限公司 | High-rise fire extinguishing fire engine and fire extinguishing method |
WO2023003099A1 (en) * | 2021-07-20 | 2023-01-26 | 주식회사 아르고스다인 | Apparatus for drone for controlling recoil from grenade launch |
-
2015
- 2015-07-10 CN CN201520500569.4U patent/CN204864620U/en active Active
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106871740A (en) * | 2017-03-30 | 2017-06-20 | 西安天鹰防务科技有限公司 | The application of barrel assemblies, shell carry frame and shell carry frame on unmanned plane |
CN107261376A (en) * | 2017-08-07 | 2017-10-20 | 沈阳金丰春航空科技有限公司 | Unmanned plane and fire-extinguishing |
CN107456683A (en) * | 2017-08-14 | 2017-12-12 | 苏州凸现信息科技有限公司 | A kind of skyscraper fire fighting device and its method of work based on unmanned plane |
CN107670201A (en) * | 2017-08-31 | 2018-02-09 | 上海机电工程研究所 | UAV system type fire extinguishing system |
CN108168371A (en) * | 2017-12-27 | 2018-06-15 | 深圳城际快机科技有限公司 | A kind of more bullet kinds of unmanned plane emit sighting device and system |
CN108454839A (en) * | 2018-04-09 | 2018-08-28 | 重庆国飞通用航空设备制造有限公司 | A kind of efficient emergency broken window multi-rotor unmanned aerial vehicle system |
CN108313279A (en) * | 2018-04-09 | 2018-07-24 | 重庆国飞通用航空设备制造有限公司 | A kind of special fire extinguishing multi-rotor unmanned aerial vehicle system of fire-fighting |
CN108313279B (en) * | 2018-04-09 | 2024-04-05 | 重庆国飞通用航空设备制造有限公司 | Fire-extinguishing multi-rotor unmanned aerial vehicle system special for fire control |
WO2020043223A1 (en) * | 2018-08-27 | 2020-03-05 | MÁTL, Roman | Mobile fire extinguishing equipment |
CN109464766A (en) * | 2018-09-14 | 2019-03-15 | 广州市华科尔科技股份有限公司 | A kind of fire-fighting method of fire-fighting unmanned plane |
CN109733876A (en) * | 2019-01-04 | 2019-05-10 | 京东方科技集团股份有限公司 | A kind of fetching device and pick and place method |
CN110270020A (en) * | 2019-07-08 | 2019-09-24 | 西安航天化学动力有限公司 | A kind of Recoilless window breaker of UAV system |
WO2023003099A1 (en) * | 2021-07-20 | 2023-01-26 | 주식회사 아르고스다인 | Apparatus for drone for controlling recoil from grenade launch |
CN113908469A (en) * | 2021-10-29 | 2022-01-11 | 亿航智能设备(广州)有限公司 | High-rise fire extinguishing fire engine and fire extinguishing method |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN204864620U (en) | Unmanned aerial vehicle carries extinguishing device | |
CN108408053A (en) | Throwing type high-altitude unmanned plane and fire-extinguishing system and its application method | |
CN105963882A (en) | Air-to-surface rocket fire extinguisher and method | |
CN105730698A (en) | Small fire extinguishing unmanned helicopter | |
CN204557841U (en) | A kind of driving of a tank simulation training system | |
CN108317893A (en) | A kind of police unmanned plane net rifle arrests module | |
CN110631418B (en) | Unmanned aerial vehicle micro weapon system with intelligent observing and hitting integrated function | |
CN208102351U (en) | A kind of ammunition throwing device based on unmanned aerial vehicle platform | |
CN101854523B (en) | Small scout and counter-strike battle robot | |
CN111442689A (en) | Multi-functional transmission trainer based on modular design | |
JP2014145531A (en) | Shooting training system | |
CN203758355U (en) | Automatic ammunition setting device for tank | |
KR101243044B1 (en) | A target for fire training of portable guided missile | |
CN209820260U (en) | Cluster type automatic signal bullet emitter based on electromagnetic percussion | |
CN208559761U (en) | Load carrier for unmanned plane | |
CN209814279U (en) | Aircraft with external fire control system | |
CN210101997U (en) | Standard ammunition throwing device for unmanned aerial vehicle | |
CN210072987U (en) | Simulation terminal for walking and chariot | |
CN207716957U (en) | A kind of police unmanned plane net rifle arrests module | |
US20160102936A1 (en) | Visual tracer and sound training device | |
CN209978711U (en) | Image shooting training system | |
CN216115622U (en) | A smoke screen bullet transmission analogue means for high imitative target | |
CN208559764U (en) | Damping device for unmanned plane | |
CN109131888A (en) | Power load-carrying members for unmanned plane | |
CN214649015U (en) | Multifunctional portable unmanned aerial vehicle |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant |